2004_rules</TIT= LE> <META http-equiv=3DContent-Type content=3D"text/html; = charset=3Diso-8859-1"> <META content=3DWord.Document name=3DProgId> <META content=3D"MSHTML 6.00.2900.2873" name=3DGENERATOR> <META content=3D"Microsoft Word 10" name=3DOriginator><LINK=20 href=3D"2004%20Rules_files/filelist.xml" rel=3DFile-List><LINK=20 href=3D"2004%20Rules_files/editdata.mso" rel=3DEdit-Time-Data><o:SmartTagType name=3D"time"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"PlaceName"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"PlaceType"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"place"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"State"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"City"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"date"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype> <STYLE>@font-face { font-family: Cancun; } @page Section1 {size: 8.5in 11.0in; margin: 1.0in 1.25in 1.0in 1.25in; = mso-header-margin: .5in; mso-footer-margin: .5in; mso-paper-source: 0; } P.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } LI.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } DIV.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } A:link { COLOR: blue; TEXT-DECORATION: underline; text-underline: single } SPAN.MsoHyperlink { COLOR: blue; TEXT-DECORATION: underline; text-underline: single } A:visited { COLOR: purple; TEXT-DECORATION: underline; text-underline: single } SPAN.MsoHyperlinkFollowed { COLOR: purple; TEXT-DECORATION: underline; text-underline: single } P { FONT-SIZE: 12pt; MARGIN-LEFT: 0in; MARGIN-RIGHT: 0in; FONT-FAMILY: = "Times New Roman"; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman"; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto } SPAN.SpellE { mso-style-name: ""; mso-spl-e: yes } SPAN.GramE { mso-style-name: ""; mso-gram-e: yes } DIV.Section1 { page: Section1 } OL { MARGIN-BOTTOM: 0in } UL { MARGIN-BOTTOM: 0in } </STYLE>  <META content=3D"C:\Program Files\Microsoft Office\Office\html.dot" = name=3DTemplate></HEAD> <BODY lang=3DEN-US style=3D"tab-interval: .5in" vLink=3Dpurple = link=3Dblue> <DIV class=3DSection1> <IMG id=3D_x0000_i1025 = height=3D150=20 src=3D"http://www.ae.uiuc.edu/aiaadbf/images/98logo.gif" = width=3D550> 2004=20 Rules and Vehicle Design <SPAN=20 style=3D"FONT-SIZE: 16pt; COLOR: red">Note: Rules are =93Draft=94 until=20 <st1:date Year=3D"2003" Day=3D"31" Month=3D"10"><SPAN=20 style=3D"FONT-SIZE: 16pt; COLOR: red">31 October = 2003</st1:date><SPAN=20 style=3D"FONT-SIZE: 24pt"><o:p></o:p> Summary:<o:p></o:p> The AIAA through the Applied Aerodynamics, = Aircraft=20 Design, Design Engineering and Flight Test Technical Committees and the = AIAA=20 Foundation invites all university students to participate in the = <SPAN=20 style=3D"FONT-FAMILY: Cancun">Cessna/ONR Student Design/Build/Fly=20 Competition. The = contest=20 will provide a real-world aircraft design experience for engineering = students by=20 giving them the opportunity to validate their analytic studies. Student teams will design, fabricate, and=20 demonstrate the flight capabilities of an unmanned, electric powered, = radio=20 controlled aircraft that can best meet the specified mission profile. = The goal=20 is a balanced design possessing good demonstrated flight handling = qualities and=20 practical and affordable manufacturing requirements while providing a = high=20 vehicle performance. To encourage innovation and maintain a = fresh design=20 challenge for each new year, the design requirements and performance = objectives=20 will be updated for each new contest year. The changes will provide new = design=20 requirements and opportunities, while allowing for application of = technology=20 developed by the teams from prior years. Cash prizes are $2500 = for=20 1st, $1500 for 2nd and $1000 for 3rd = place. The=20 winning teams will be invited to present their designs at the 2004 AIAA = Flight=20 Test & Evaluation conference. Judging:<o:p></o:p> Students must design, document, fabricate, = and=20 demonstrate the aircraft they determine as best capable of achieving the = highest=20 score on the specified mission profile(s). Flight scores will be based = on the=20 demonstrated mission performance obtained during the contest. Each team must also submit a written = Design Report.=20 A maximum of 100 points will be awarded for the team design report. = Scores for=20 the written reports will be announced at the beginning of the = fly-off. Each aircraft will have computed a Rated = Aircraft=20 Cost, reflecting the complexity/technology of the design. The overall team score is a combination of = the=20 Design Report, Rated Aircraft Cost and Flight scores. The team with the = highest=20 overall team score will be declared the winner. Contest = Site:<o:p></o:p> Host for the competition = will be the=20 Cessna Aircraft Company. The fly-off will be held at The Cessna Pawnee = East=20 Field at <st1:place><st1:City>Wichita</st1:City>=20 <st1:State>Kansas</st1:State></st1:place>. You can check on weather historical = conditions at=20 www.weatherbase.com or www.weatherunderground.com. Team=20 Requirements:<o:p></o:p> All team members (except for a = pre-approved=20 designated pilot) must be full time students at an accredited University = or=20 College and student members of the AIAA. The team must be composed of = both under=20 classmen and upper classmen, with at least 1/3 of the members being = under=20 classmen (Freshman, Sophomores or Juniors). The pilot must be an AMA=20 (<st1:place><st1:PlaceType>Academy</st1:PlaceType> of = <st1:PlaceName>Model=20 Aeronautics</st1:PlaceName></st1:place>) member. Teams may use a = non-university=20 member for the pilot if desired. We will also provide qualified pilots = on the=20 contest day for any teams who are unable to have their pilot attend. Past Year=20 Reports:<o:p></o:p> The top scoring report from the past years = competition will be available for reference on the contest web site. The = team=20 with the top scoring report from this years contest will be required to = submit=20 an electronic copy of their report following the competition, which will = be=20 placed on the contest web site for the next years competition. Sponsorship:<o:p></o:p> Teams may solicit and accept sponsorship = in the form=20 of funds or materials and components from commercial organizations. All = <SPAN=20 style=3D"COLOR: red">design, analysis and=20 fabrication of the contest entry is the sole = responsibility of the=20 student team members. Schedule:<o:p></o:p> A completed electronic entry form is due = to the=20 contest administrator on or before <st1:date Year=3D"2003" Day=3D"31"=20 Month=3D"10">31 October=20 2003</st1:date>. The entry form for the DBF is different = than that=20 used for all other AIAA student competitions.<SPAN=20 style=3D"mso-spacerun: yes"> The DBF entry form is a = MS-Word file and=20 can be found on the contest web site. It must be submitted by e-mail to = the=20 contest administrator at <A=20 href=3D"mailto:gregory.s.page@nrl.navy.mil">gregory.s.page@nrl.navy.mil</= A> . Be=20 sure to include the Phone and FAX number for your team advisor and at = least one=20 student contact so we may reach you in case of any last minute problems = or=20 changes. All teams are = required to=20 provide two point-of-contact e-mail addresses with their contest = application,=20 one of which must be the teams advisor. =20 <I=20 style=3D"mso-bidi-font-style: normal">It is the teams responsibility to = make sure=20 the e-mail contact addresses they supply remain active during the entire = period=20 from entry to the close of the competition, as e-mail will be the = primary means=20 to provide information and updates.<o:p></o:p> Please=20 Note: the Entry = Name may not=20 be changed once the form is submitted, but must be retained and used in = all=20 reports and correspondence during the competition year. Written reports (5=20 hard copies, electronic reports will not be accepted), = are due to=20 the contest administrator by COB <st1:date Year=3D"2004" Day=3D"9"=20 Month=3D"3">9 March = 2004</st1:date>.<SPAN=20 style=3D"mso-spacerun: yes"> Reports will be judged =93as=20 received=94, no =93corrections/additions/page = changes=94 will=20 be made by the organizers so check your reports carefully before sending = them. COB is taken as = <st1:time=20 Hour=3D"17" Minute=3D"0">5 pm</st1:time> local time at the address = provided for=20 delivery of the written reports. = Scores for the written reports will be announced at the beginning = of the=20 fly-off. (A note=20 primarily for foreign entrants but also allowed for domestic teams. If sending the report by = courier is=20 prohibitive you may send it electronically to a commercial = printer (<SPAN=20 class=3DSpellE>KINKO=92s comes to mind) local to the report = submission=20 address and have them print/collate and DELIVER the reports to meet the=20 deadline. No deadline = exceptions=20 will be made, but this may be easier than international courier=20 service.)<o:p></o:p> The contest is scheduled for <SPAN=20 style=3D"COLOR: red">23-25 April 2004.<SPAN=20 style=3D"mso-spacerun: yes"> The competition will run from = <st1:time=20 Hour=3D"12" Minute=3D"0">noon</st1:time> to <st1:time Hour=3D"17"=20 Minute=3D"0">5PM</st1:time> on Friday, and <st1:time Hour=3D"8" = Minute=3D"0">8AM to=20 5PM</st1:time> on Saturday and Sunday. Final awards will be presented at = the end=20 of Sunday's competition. All teams are encouraged to stay and attend the = awards=20 presentations on Sunday. Please note that tech inspections will be = available=20 on Friday 23 April. Teams are = encouraged=20 to be prepared to have your plane inspected on Friday. Inspections will = also be=20 available on Saturday, but waiting until Saturday to go through tech may = mean=20 that your team will miss one or more rounds through the flight queue. If = we have=20 a full turnout you may not be able to get in a full set of scoring = flights=20 unless you are "ready to fly" at every opportunity. Late entries will <SPAN=20 style=3D"COLOR: red">NOT be accepted.<SPAN=20 style=3D"mso-spacerun: yes"> Late or incomplete report = submissions=20 will NOT be judged. Teams who = do not=20 submit the required written reports will NOT be=20 allowed to fly. It is the = teams=20 responsibility to assure that all deadlines are met, as they will be = <SPAN=20 style=3D"COLOR: red">strictly enforced. Communications:<o:p></o:p> The contest administration will maintain a = World=20 Wide Web site containing the latest information regarding the contest = schedules,=20 rules, and participating teams. The contest web site will also contain a = list of=20 potential suppliers for materials and equipment available to build an = entry. The=20 contest web site is located at: <SPAN=20 style=3D"COLOR: = blue">http://www.aae.uiuc.edu/aiaadbf<o:p></o:p> Later in the academic year, the website = will be=20 moved to <SPAN=20 style=3D"COLOR: blue">http://www.ae.uiuc.edu/~aiaadbf Questions regarding the contest, = schedules, or rules=20 interpretation may be sent to the contest administrator by e-mail = at: <SPAN=20 style=3D"COLOR: blue">gregory.s.page@nrl.navy.mil<o:p></o:p> The contest administrator will provide = e-mail copies=20 of questions received and their answers to all teams of record. Written reports (only) should be sent to = the chief=20 of scoring at: AIAA = Design/Build/Fly=20 Contest/Report Judging Kelly Laflin Cessna=20 Aircraft Company Dept. 363 P Cessna Aircraft Company 5800 = East Pawnee=20 Wichita, KS 67218 316-831-2247<o:p></o:p> Aircraft Requirements -=20 General<o:p></o:p> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">The=20 aircraft may be of any configuration except rotary wing or = lighter-than-air.=20 <LI class=3DMsoNormal=20 style=3D"COLOR: black; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto; mso-list: l11 level2 lfo3; tab-stops: list = 1.0in"><SPAN=20 style=3D"COLOR: windowtext">No payload may be carried internal to = the wing=20 proper. Payload in the "fuselage" may be carried in the area where = the wing=20 carry-over structure passes. For blended-wing configurations, = the=20 "fuselage" is defined to be the inner most 9=20 inch of semi-span, the remainder is "wing" for payload=20 considerations. <o:p></o:p> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Must=20 be propeller driven and electric powered with an unmodified = over-the-counter=20 model electric motor. May use multiple motors and/or propellers. May = be=20 direct drive or with gear or belt reduction.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">All=20 motors must be from the Graupner=20 or Astro Flight = families of=20 brushed electric motors, only =20 (motor should have manufacturers label visible to the judges = during=20 the technical inspection).=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">For=20 safety, each aircraft will use a commercially produced propeller. = Teams may=20 modify the propeller diameter by clipping the tip, and may paint the = blades=20 to balance the propeller. = No=20 other modifications to the propeller are allowed.<SPAN=20 style=3D"mso-spacerun: yes"> Commercial ducted fan = units are=20 allowed.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Motors=20 and batteries will be limited to a maximum of 40 Amp current draw by = means=20 of a 40 Amp fuse (per motor or pack) in the line from the positive = battery=20 terminal to the motor controller. Only ATO or blade style plastic = fuses may=20 be used. ("Maxi" size Slow Blow, 1.15"x0.85". Available online=20 www.Mcmaster.com part #7460K51 $1.66 each)=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Must=20 use over the counter NiCad batteries. = For safety,=20 battery packs must have shrink-wrap or other protection over all = electrical=20 contact points. The individual cells must be commercially available, = and the=20 manufacturers label must be readable (i.e. clear shrink wrap = preferred). All=20 battery disconnects must be "fully insulated" style connectors.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Maximum=20 battery pack weight is 5 lb. <st1:place>Battery</st1:place> pack = must power=20 propulsion and payload systems only. Radio Rx and servos MUST = be on a=20 separate battery pack. Batteries may not be changed or charged = between=20 sorties during a flight period.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Aircraft=20 and pilot must be AMA legal. This means that the aircraft TOGW = (take-off=20 gross weight with payload) must be less than 55 lb, and the = pilot must=20 be a member of the AMA.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Since=20 this is an AMA sanctioned event, the team must submit proof that the = aircraft has been flown prior to the contest date (in flight photo) = to the=20 technical inspection team. Contest supplied qualified pilots will be = available to teams who require them.=20 <LI class=3DMsoNormal=20 style=3D"COLOR: red; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto; mso-list: l11 level2 lfo3; tab-stops: list = 1.0in">Teams=20 will present a completed a signed (by the teams faculty advisor) = copy of=20 their Rated Aircraft Cost worksheet to the judges during technical=20 inspection for verification. The Rated Aircraft Cost assigned at the = technical inspection will be used for the competition and may not be = modified during the event. <o:p></o:p></LI></UL></UL> Aircraft Requirements -=20 Safety<o:p></o:p> All vehicles will undergo a safety = inspection by a=20 designated contest safety inspector prior to being allowed to make any=20 competition or non-competition (i.e. practice) flight. All decisions of = the=20 safety inspector are final. Safety inspections will include the = following as a=20 minimum. <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l1 level2 lfo6; tab-stops: list 1.0in">Physical=20 inspection of vehicle to insure structural integrity. = </LI></UL></UL> <OL type=3D1> <OL type=3D1> <OL type=3D1> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 all components adequately secured to vehicle. Verify all fasteners = tight=20 and have either safety wire, locktite = (fluid) or=20 nylock nuts.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 propeller structural and attachment integrity.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Visual=20 inspection of all electronic wiring to assure adequate wire gauges = and=20 connectors in use. Teams must notify inspector of expected maximum = current=20 draw for the propulsion system.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Radio=20 range check, motor off and motor on.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 all controls move in the proper sense.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Check=20 general integrity of the payload system. </LI></OL></OL></OL> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l7 level2 lfo12; tab-stops: list 1.0in">Structural=20 verification. All aircraft will be lifted with one lift point at = each wing=20 tip to verify adequate wing strength (this is "roughly" equivalent = to a 2.5g=20 load case) and to check for vehicle cg location. <SPAN=20 style=3D"COLOR: red">Both upright and inverted wing lift tests will = be=20 performed. = Teams must=20 mark the expected empty and loaded cg locations on the exterior of = the=20 aircraft fuselage. Special provisions will be made at the time of = the=20 contest for aircraft whose cg does not fall within the wing tip = chord. This=20 test will be made with the aircraft filled to its maximum = payload=20 capacity.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l7 level2 lfo12; tab-stops: list 1.0in">Radio=20 fail-safe check. All aircraft radios must have a fail-safe mode that = is=20 automatically selected during loss of transmit signal. The fail-safe = will be=20 demonstrated on the ground by switching off the transmit radio. = During fail=20 safe the aircraft receiver must select: </LI></UL></UL> Throttle closed Full up elevator = Full=20 right rudder Full right (or left) aileron Full Flaps down (if so = equipped) During Fail = Safe the=20 payload release system must NOT activate.<o:p></o:p> The radio Fail Safe provisions = will be=20 strictly enforced.<o:p></o:p> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l8 level2 lfo15; tab-stops: list 1.0in">All=20 aircraft must have a mechanical motor arming system separate from = the=20 onboard radio Rx switch. This MUST = be the=20 contest specified "blade" style fuse. This device must be located so = it is=20 accessible by a crewmember standing ahead of the = propeller(s)=20 for pusher aircraft, and standing behind the = propeller(s) for=20 tractor aircraft (i.e. the crew member must not reach across the = propeller=20 plane to access the fuse). The "Safety Arming Device" will be in = "Safe" mode=20 for all payload changes. The aircraft Rx should always be powered on = and the=20 throttle verified to be "closed" before activating the motor arming=20 switch. Fuses MUST be = accessible from outside the aircraft and act as the "<SPAN=20 class=3DSpellE>safeing" device. </LI></UL></UL> <st1:place><SPAN=20 style=3D"FONT-SIZE: 13.5pt">Mission</st1:place><SPAN=20 style=3D"FONT-SIZE: 13.5pt"> Profile:<o:p></o:p> Teams must complete the flight missions as = outlined=20 in the mission matrix below. = Teams=20 will have a maximum of <SPAN=20 style=3D"FONT-SIZE: 14pt; mso-bidi-font-size: 12.0pt">5 = flight=20 attempts. A flight attempt is defined as advancing the throttle = =93stick=94 for=20 take-off. The best Single Flight Score from each of = 2=20 different mission types will be summed for the team's = Total Flight=20 Score. In the event that, due to time or = facility=20 limitations, it is not possible to allow all teams to have the maximum = number of=20 flight attempts, the contest committee reserves the right to ration = and/or=20 schedule flights. The exact determination of how to ration flights will = be made=20 on the contest day based on the number of entries, weather, and field=20 conditions.<o:p></o:p> Each team's overall score will be computed = from=20 their Written Report Score, Total Flight Score, and = the=20 Rated Aircraft Cost using the formula: SCORE =3D Written = Report Score *=20 Total Flight Score Rated Aircraft Cost<o:p></o:p> <A=20 name=3DOLE_LINK1></A><st1:place><SPAN=20 style=3D"FONT-SIZE: 18pt">Mission</st1:place><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> = Task=20 Matrix<o:p></o:p> <DIV align=3Dcenter> <TABLE class=3DMsoNormalTable=20 style=3D"WIDTH: 5.25in; mso-cellspacing: .6pt; mso-padding-alt: 5.4pt = 5.4pt 5.4pt 5.4pt"=20 cellSpacing=3D1 cellPadding=3D0 width=3D630 border=3D1> <TBODY> <TR style=3D"mso-yfti-irow: 0"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: = OLE_LINK1"><st1:City><st1:place><SPAN=20 style=3D"mso-bookmark: = OLE_LINK1">Mission</st1:place></st1:City><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Description</TD></TR> <TR style=3D"mso-yfti-irow: 1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> </TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">General Mission=20 Information<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must fit in a 2-ft wide by = 1-ft=20 high by 4-ft long (interior dimensions) box.<SPAN=20 style=3D"mso-spacerun: yes"> Note: The aircraft does = not need=20 to =93fold=94 to fit in the box, but may employ =93plug-in=94 = joints for rapid=20 assembly/disassembly. = All=20 electrical connections should be keyed so they cannot be=20 misassembled. Tape = may be=20 used as a non-structural =93latch=94 to hold components in place, = such as=20 taping a wing joint when using a plug-in spar arrangement to keep = the wing=20 from sliding loose. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Teams must select one of the = following=20 missions for each flight. =20 Teams may select a different mission for each of their = scoring=20 flight attempts. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Take-off distance is 150 ft wheels = off the=20 runway. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On landing the aircraft must land = on the=20 runway (but may roll off) to obtain a score for that = flight. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>All payloads must be adequately = secured=20 using mechanical means. = Tape=20 and Velcro are not acceptable forms of restraint. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum mission time is = <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><SPAN=20 style=3D"FONT-SIZE: 14pt; mso-bidi-font-size: = 12.0pt">10=20 minutes.</TD></TR> <TR style=3D"mso-yfti-irow: 2"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Fire = Fight<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Heavy=20 Lift/Slow Flight<o:p></o:p></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Fire Bomber DF =3D=20 2.0<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft will begin the mission = time=20 empty. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The flight mission will consist of = two=20 sorties. (1) Aircraft will be loaded, take-off, dump its water = load=20 during the downwind leg, and return to land. (2) Aircraft will = be=20 reloaded, take-off, dump its water load during the downwind leg, = and=20 return to land. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum allowed aircraft water = capacity is=20 4 liters. <I=20 style=3D"mso-bidi-font-style: normal">(Aircraft=20 will be emptied then filled to overflow during the tech = inspection.<SPAN=20 style=3D"mso-spacerun: yes"> Total volume must be 4 = liters or=20 less.) <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Teams will load the aircraft during = the=20 mission from four 2-liter plastic =93soda=94 bottles.<SPAN=20 style=3D"mso-spacerun: yes"> Teams may use gravity = loading or=20 =93pumped=94 loading. = Soda=20 bottles may NOT be pressurized to assist loading. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On all laps flown the aircraft must = complete a single 360o turn in the direction = opposite of=20 the base and final turns on the downwind leg of each lap. = <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Water may only be dumped during the = downwind leg between the upwind and downwind turn = markers/flags.<SPAN=20 style=3D"mso-spacerun: yes"> <I=20 style=3D"mso-bidi-font-style: normal">Aircraft must fly slow = enough to allow=20 sufficient time for the water to be emptied. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum dump orifice diameter is = 0.5 inch.=20 (Measured at the = exit so it=20 may be easily verified during the tech inspection). <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The pilot must call =93Dump = On=94 and=20 =93Dump Off=94 so the observer judge can easily verify that the = water dump is=20 restricted to the downwind leg. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"COLOR: red; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Early or = Late=20 water dumping, including inadvertent release of water during a = hard=20 landing, will incur a 3-min time penalty per = occurrence. Excessive=20 water spillage during loading will incur a 1-min time penalty per=20 infraction. The = flight line=20 judge will notify the team of the penalty at the time of the=20 infraction. Gross = and/or=20 deliberate spillage will disqualify the flight but will count as = one of=20 the teams=92 flight attempts. A 3-min time penalty will be = added if=20 the aircraft is not empty on landing after the final=20 lap.<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>A time penalty of 3 minutes will be = added=20 for an incomplete second lap. =20 If the second lap is not attempted or the 360o = turn is=20 not completed the second lap will be timed as = =93incomplete.=94 <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The weight of the water will be = determined=20 by the starting and ending weight of the team=92s ground-based = storage=20 =93tanks,=94 taken when entering and leaving the flight = box. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]><B=20 style=3D"mso-bidi-font-weight: normal">Single Flight Score = is: DF=20 * Lbs_Water / <SPAN=20 class=3DSpellE>Mission_Time</TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"></TR> <TR style=3D"mso-yfti-irow: 3; mso-yfti-lastrow: yes"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: = OLE_LINK1">Ferry<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">High Speed=20 Flight<o:p></o:p></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Ferry DF =3D=20 1.0<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must take-off, complete = four laps,=20 and land. The = aircraft will=20 have no water payload for this flight <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On all laps flown the aircraft must = complete a 360o turn in the direction opposite of the = base and=20 final turns on the downwind leg of each lap. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]><B=20 style=3D"mso-bidi-font-weight: normal">Single Flight Score = is: DF=20 / Mission_time</TD><SPAN=20 style=3D"mso-bookmark: = OLE_LINK1"></TR></TBODY></TABLE></DIV><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> "Mission Flight Time" is the time from = when the=20 official calls "go" until the aircraft comes to a <SPAN=20 style=3D"COLOR: red">complete stop <B=20 style=3D"mso-bidi-font-weight: normal"><SPAN=20 style=3D"COLOR: red">PAST the starting line at the = completion of=20 all laps. Aircraft that = run off the=20 runway before reaching the start line may be carried to the line to end = the=20 time. Aircraft that are = damaged may=20 NOT be carried to the line to end the time, but will instead have the = time end=20 where the aircraft stops with the last lap scored as = =93incomplete.=94 For aircraft not completing the full = number of laps=20 specified for a mission, a penalty of 3 minutes will be added to the = aircraft's=20 measured "Total Mission Time" = for=20 each lap not = completed.<SPAN=20 style=3D"mso-spacerun: yes"> For example, if an aircraft = completes=20 only 3 laps of a 4 lap mission in 5 minutes, the "Total Mission Time" = would be:=20 5 minutes + 1 incomplete laps @ 3 minutes each =3D 8 minutes. <SPAN=20 style=3D"FONT-SIZE: 18pt">Aircraft Cost Model<o:p></o:p> Rated = Aircraft=20 Cost, $ (Thousands) =3D (A*MEW + B*REP + C*MFHR)/1000 <DIV align=3Dcenter> <TABLE class=3DMsoNormalTable=20 style=3D"WIDTH: 409.8pt; mso-cellspacing: .6pt; mso-padding-alt: 5.4pt = 5.4pt 5.4pt 5.4pt"=20 cellSpacing=3D1 cellPadding=3D0 width=3D683 border=3D1> <TBODY> <TR style=3D"mso-yfti-irow: 0"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> <SPAN=20 class=3DSpellE>Coef.</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Description</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Value</TD></TR> <TR style=3D"mso-yfti-irow: 1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> A</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturers Empty Weight Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $300 <SPAN=20 style=3D"COLOR: red">(NEW)<o:p></o:p></TD></TR> <TR style=3D"mso-yfti-irow: 2"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> B</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Rated Engine Power Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $1500</TD></TR> <TR style=3D"mso-yfti-irow: 3"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> C</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturing Cost Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $20 / hour</TD></TR> <TR style=3D"mso-yfti-irow: 4"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> MEW</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturers Empty Weight</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Actual airframe weight [lb] with all=20 flight and propulsion batteries but without any = payload.</TD></TR> <TR style=3D"mso-yfti-irow: 5"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> REP</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Rated Engine Power</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> (1+.25*(# engines-1)) * Total=20 <st1:place>Battery</st1:place> Weight=20 [lbs]<o:p></o:p> "Total = <st1:place>Battery</st1:place>=20 Weight" will be the weight of the propulsion battery = pack(s) as=20 determined by the judges scale during = technical=20 inspection. Total propulsion battery pack weight may not exceed 5 = lb, but=20 it may be lighter.</TD></TR> <TR style=3D"mso-yfti-irow: 6; mso-yfti-lastrow: yes"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> MFHR</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturing Man Hours</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Prescribed assembly hours by WBS (Work Breakdown = Structure). MFHR =3D S WBS = hours WBS 1.0=20 Wing(s): = (NEW)<o:p></o:p> 10 hr/ft^2 Wing Span * Chord * # wings Wing Span is = longest=20 distance perpendicular to fuselage axis on any wing.<SPAN=20 style=3D"mso-spacerun: yes"> Chord is maximum exposed = wing=20 chord on any wing. = For a=20 blended wing-body, exposed wing starts 9 inch out from the body=20 centerline. 5 hr * <SPAN=20 class=3DSpellE>control_function_multiplier ailerons =3D = 1 <SPAN=20 class=3DSpellE>flaperons =3D 1.5 ailerons + flaps =3D = 2 ailerons +=20 spoilers =3D 2 ailerons + flaps + spoilers =3D 3 WBS 2.0 = Fuselage=20 (NEW)<o:p></o:p> 20 hr/ft^3 Body Length x Width x Height Length is = maximum=20 body length. Width = is maximum=20 body width. Height = is maximum=20 body height (does not include landing gear height).<SPAN=20 style=3D"mso-spacerun: yes"> Maximum body width and = maximum=20 body height may occur at different fuselage locations. For = a=20 blended wing-body, body width is fixed at 18 inch. Note: = Maximum=20 length of the body is defined to be the longest longitudinal = length=20 possible to measure on the aircraft, and may include spinner and = part of=20 vertical or horizontal surfaces. WBS 3.0=20 Empennage<o:p></o:p> 5 hr/Vertical Surface (Any vertical surface, including = winglets,=20 struts, end plates, ventral etc) with no active control 10=20 hr/Vertical Surface (Any vertical surface) with an active=20 control 10 hr/Horizontal Surface. A horizontal surface is a = "wing"=20 if it is more than 25% of the span of the greatest span horizontal = surface.) A "V" tail is considered to be a Vertical surface without = control (5=20 hr) plus a horizontal surface with controls (10 hr), for a total = of 15=20 hr. WBS 4.0 = Flight=20 Systems<o:p></o:p> 5 hr/servo or motor controller WBS 5.0 = <SPAN=20 style=3D"COLOR: red">(Deleted)<o:p></o:p> </TD></TR></TBODY></TABLE></DIV> <o:p></o:p> Rated Aircraft Cost must be = supplied=20 when the aircraft enters the technical inspection. The RAC worksheet = must be=20 signed by the team advisor. RAC may = not be=20 changed during the competition unless it is determined by the contest = officials=20 to be inaccurate or inappropriate. The contest officials reserve the = right to=20 audit and revise the RAC for omissions or errors at any time. <SPAN=20 style=3D"FONT-SIZE: 18pt">General Mission Specification and=20 Notes:<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft are to remain assembled while = waiting in=20 the queue. Teams will = install the=20 propulsion batteries once reaching the <B=20 style=3D"mso-bidi-font-weight: normal">3rd =93On=20 Deck=94 position (i.e. when the aircraft is 3rd in = the=20 queue, the team must begin to install the batteries). <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft may = not=20 have any work performed in the starting line queue, other than as = specified=20 above at the 3rd On Deck position. Aircraft propulsion = batteries may=20 be left out of the aircraft when in line. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft batteries may be charged while = the=20 aircraft is in the queue IF AND ONLY = IF the=20 batteries are removed from the aircraft. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The aircraft propulsion system(s) must be = disarmed or "safed" during any time when = crew members=20 are preparing the aircraft. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum flight support crew is: pilot, = observer,=20 and 3 ground crew. Only the designated ground crew may reload the = aircraft=20 payload . Pilot and observer may be members of the ground crew, provided = total=20 ground crew size remains 3 people. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Observer and all ground crew must be=20 students. <SPAN=20 style=3D"COLOR: red">Only the pilot may be a non-student. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The upwind turn will be made after = passing the=20 upwind pylon. The downwind turn will be made after passing the downwind = pylon.=20 Upwind and downwind pylons will be 500 ft from the starting line. = Aircraft must=20 be "straight and level" when passing the pylon before initiating the = turn. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must land on the paved portion = of the=20 runway. Aircraft may "run-off" the runway during roll-out. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>After landing, aircraft <SPAN=20 style=3D"COLOR: red">may taxi back to the starting line. = Alternatively,=20 aircraft may be carried back to the starting line; however, the team may = not=20 leave the pit area to retrieve the aircraft until the aircraft has come = to a=20 complete stop, and they are signaled it is "Ok" to retrieve the aircraft = by the=20 flight line judge. <I=20 style=3D"mso-bidi-font-style: normal">Aircraft experiencing damage = during landing=20 will be considered to have completed their flight where they come to = rest and my=20 not be =93carried=94 to the starting line to =93complete=94 a = lap. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft will be considered to have only = minor=20 damage if they can be repaired and presented as flight worthy within = 30=20 minutes of the end of that flight period. Aircraft with only minor = damage=20 will be credited with their full Single Flight Score. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft that can be repaired during the=20 competition, but not within 30 minutes of the flight period, will NOT be = credited with a score for that flight period. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Flight altitude must be sufficient for = safe=20 terrain clearance and low enough to maintain good visual contact with = the=20 aircraft. Decisions on safe flight altitude will be at the discretion of = the=20 flight line judges and all rulings will be final. Additional information is included in the = <A=20 href=3D"http://www.ae.uiuc.edu/2003%20DBF/2003_faq.html">FAQ</A> = (Frequently Asked=20 Questions). Protest=20 Procedures<o:p></o:p> Submitting a protest against a competing = team is a=20 serious matter and will be treated as such. Teams may submit a protest = to the=20 Contest Administrator at any time during the competition. Protests must = be=20 submitted in writing and signed by the team advisor (if present at the=20 competition) or the team captain if a faculty advisor is not present. = Protests=20 will be posted for all teams to review. If the protest is rejected, the submitting = team(s)=20 will forfeit one of their remaining flight attempts. If all flight = attempts have=20 been used, the team(s) will forfeit their lowest Single Flight = score. Protests and the appropriate penalty = (ranging from a=20 requirement to repeat a flight for minor infractions to disqualification = from=20 the contest for deliberate attempts to misinform officials or violate = the=20 contest rules) will be decided by the Contest Administrator and the = Contest=20 Director, in consultation with other Contest Officials. The decision of = the=20 Contest Administrator and Contest Director is final. NEW<SPAN=20 style=3D"FONT-SIZE: 13.5pt"> for This Year<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Inverted wing tip lift test was added <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft missions are revised. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Missions have different difficulty = factors=20 applied. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must fit in a specified size = shipping=20 container, but assembly time is NOT part of the mission scoring. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>RAC formulas have been rescaled. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>3-view drawing in report must be = on an 11=20 x 17 inch page for easier reading by judges Design = Report:<o:p></o:p> Each team will submit a judged design = report as=20 outlined below. The submission date is contained in the schedule section = of this=20 document. Reports must be bound. (Simple spiral bindings are sufficient = and=20 preferred; 3-ring binders are not allowed.) All information used for = scoring=20 must be in the outlined sections. Reports exceeding the total page = limit will=20 be scored as "1 of 100". Appendices may not be included. All reports will be space and one half, = 10-pt Arial=20 font. Tables and figures will also be 10-pt Arial font. Margins are 1 = inch on=20 all sides. Report pages will be 8 1/2 x 11 inch with the exception of = the=20 drawing package. The = drawing=20 package may be 11 x 17 inch pages. =20 The 3-view drawing must be on = an 11 x 17=20 inch page. Absolute maximum page count for the report = is=20 60 pages, including text, = tables, and=20 figures (cover/title page and table of contents is extra). Drawing = package may=20 not comprise more than 5 of the pages of the report page limit. All figures must be either half (1/2) page = or full=20 (1) page format. No exceptions. Please note that the judges will be = using this=20 same report outline for evaluating reports. ALL items listed will = be=20 expected to be present, easy to locate and identify and well documented = in the=20 report for a maximum score.<o:p></o:p> <SPAN=20 style=3D"FONT-SIZE: 16pt; mso-bidi-font-size: 13.5pt">Design=20 Report<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">1.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Executive Summary: (5 points): Provide a = summary of=20 the development of your design. This should be a narrative description=20 highlighting the major areas in the development process for your final=20 configuration and a broad description of the range of design = alternatives=20 investigated. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">2.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Management Summary (5 points): Describe the=20 organization of the design team. Provide a chart of design personnel and = assignment areas. Include a (single) milestone chart showing planned and = actual=20 timing of major elements of the design process, including as a minimum = the=20 conceptual design stage, preliminary design stage, detailed design = stage, flight=20 testing and report preparation periods. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">3.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Conceptual Design (20 points): Describe the = key=20 elements of the mission requirements (problem statement).<SPAN=20 style=3D"mso-spacerun: yes"> Document the alternative = configuration=20 concepts (e.g. biplane, canard, flying wing, pusher -Vs tractor, number = of=20 engines etc.) investigated during the conceptual design stage and the = reason why=20 each concept was considered. Describe and document the numerical figures = of=20 merit (FOM's) used to screen competing = concepts, and=20 the mission feature each FOM was selected to support. Rated = Aircraft=20 Cost should be one of the FOM=92s<SPAN=20 style=3D"mso-spacerun: yes"> used during the screening = process.<SPAN=20 style=3D"mso-spacerun: yes"> Numerical data need not be = extensive at=20 this stage, but should include as a minimum: a final ranking chart = giving the=20 quantitative value of each design for each FOM. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">4.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Preliminary Design (30 points): Document the = design=20 parameter and sizing trades investigated during the preliminary design = stage,=20 and why each was felt to be important to the mission. Describe the = analysis=20 methods used. Describe the mission model used and the predicted = performance.=20 Provide estimates of the aircraft lift, drag and stability = characteristics.<SPAN=20 style=3D"mso-spacerun: yes"> Document the design = optimization and=20 trade studies conducted and their results. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">5.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Detail Design (15 points for discussion items, = 10 points=20 for drawing package, 25 points total for the section): Document = component=20 selection and systems architecture selection. Include your final = competition=20 aircraft's Rated Aircraft Cost using the contest supplied = cost=20 model. RAC table should = include all=20 input parameter, intermediate and final computation. Include a = table=20 giving data for the sized aircraft. =20 A copy of this table must be posted by the team at their = =93pit=94 area=20 (poster board). The table = should=20 include; Geometry: length, span, height, wing area, Aspect Ratio, = control=20 volumes Performance: CL max, L/D max, maximum Rate of Climb, stall = speed,=20 maximum speed, take-off field length (two sets, empty and gross=20 weight) Weight Statement (airframe, propulsion system, control = system,=20 payload system, payload, empty weight, gross weight) Systems (radio = used,=20 servos used, battery configuration used, motor used, propeller = (nominal), gear=20 ratio (if used) The Drawing = Package will=20 be included with this section and must contain as a = minimum a=20 3-view drawing of the design in sufficient detail to indicate aircraft = size and=20 configuration; primary structure component size and location; payload = size,=20 location and restraint method; and location of propulsion and flight = control=20 system components. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">6.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Manufacturing Plan and processes (10=20 points): Document the process selected for manufacture of major = components=20 and assemblies of the final design. Detail the manufacturing processes=20 investigated, and describe the FOM's used = (including=20 but not limited to: availability, required skill levels and cost) to = screen=20 competing concepts. Describe the analytic methods (cost, skill matrix,=20 scheduling time lines) used to select the final set of manufacturing = processes.=20 Include a manufacturing milestone chart showing scheduled event = timings. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">7.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Testing Plan (5 points): Detail testing = objectives,=20 schedules, check-lists, results and any lessons learned for component = and full=20 aircraft testing, both static and dynamic (ie. in=20 flight). <IMG id=3D_x0000_i1026 = height=3D299=20 src=3D"http://www.ae.uiuc.edu/aiaadbf/images/98course.gif" width=3D480 = border=3D0> <DIV class=3DMsoNormal style=3D"TEXT-ALIGN: center" align=3Dcenter> <HR align=3Dcenter width=3D"100%" SIZE=3D3> </DIV> [<A=20 href=3D"http://www.ae.uiuc.edu/aiaadbf/2004_rules.html#top">Top</A>] [<A = href=3D"http://www.ae.uiuc.edu/aiaadbf/index.html">AIAA Student = Design/Build/Fly=20 Competition homepage</A>] [<A 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From: Subject: 2004_rules Date: Tue, 2 May 2006 13:50:29 -0500 MIME-Version: 1.0 Content-Type: multipart/related; type="text/html"; boundary="----=_NextPart_000_007F_01C66DEF.5F69FA30" X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 This is a multi-part message in MIME format. ------=_NextPart_000_007F_01C66DEF.5F69FA30 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Content-Location: http://www.ae.uiuc.edu/aiaadbf/2004_rules.html 2004_rules</TIT= LE> <META http-equiv=3DContent-Type content=3D"text/html; = charset=3Diso-8859-1"> <META content=3DWord.Document name=3DProgId> <META content=3D"MSHTML 6.00.2900.2873" name=3DGENERATOR> <META content=3D"Microsoft Word 10" name=3DOriginator><LINK=20 href=3D"2004%20Rules_files/filelist.xml" rel=3DFile-List><LINK=20 href=3D"2004%20Rules_files/editdata.mso" rel=3DEdit-Time-Data><o:SmartTagType name=3D"time"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"PlaceName"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"PlaceType"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"place"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"State"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"City"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype><o:SmartTagType=20 name=3D"date"=20 namespaceuri=3D"urn:schemas-microsoft-com:office:smarttags"></o:SmartTagT= ype> <STYLE>@font-face { font-family: Cancun; } @page Section1 {size: 8.5in 11.0in; margin: 1.0in 1.25in 1.0in 1.25in; = mso-header-margin: .5in; mso-footer-margin: .5in; mso-paper-source: 0; } P.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } LI.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } DIV.MsoNormal { FONT-SIZE: 12pt; MARGIN: 0in 0in 0pt; FONT-FAMILY: "Times New Roman"; = mso-style-parent: ""; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman" } A:link { COLOR: blue; TEXT-DECORATION: underline; text-underline: single } SPAN.MsoHyperlink { COLOR: blue; TEXT-DECORATION: underline; text-underline: single } A:visited { COLOR: purple; TEXT-DECORATION: underline; text-underline: single } SPAN.MsoHyperlinkFollowed { COLOR: purple; TEXT-DECORATION: underline; text-underline: single } P { FONT-SIZE: 12pt; MARGIN-LEFT: 0in; MARGIN-RIGHT: 0in; FONT-FAMILY: = "Times New Roman"; mso-pagination: widow-orphan; = mso-fareast-font-family: "Times New Roman"; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto } SPAN.SpellE { mso-style-name: ""; mso-spl-e: yes } SPAN.GramE { mso-style-name: ""; mso-gram-e: yes } DIV.Section1 { page: Section1 } OL { MARGIN-BOTTOM: 0in } UL { MARGIN-BOTTOM: 0in } </STYLE>  <META content=3D"C:\Program Files\Microsoft Office\Office\html.dot" = name=3DTemplate></HEAD> <BODY lang=3DEN-US style=3D"tab-interval: .5in" vLink=3Dpurple = link=3Dblue> <DIV class=3DSection1> <IMG id=3D_x0000_i1025 = height=3D150=20 src=3D"http://www.ae.uiuc.edu/aiaadbf/images/98logo.gif" = width=3D550> 2004=20 Rules and Vehicle Design <SPAN=20 style=3D"FONT-SIZE: 16pt; COLOR: red">Note: Rules are =93Draft=94 until=20 <st1:date Year=3D"2003" Day=3D"31" Month=3D"10"><SPAN=20 style=3D"FONT-SIZE: 16pt; COLOR: red">31 October = 2003</st1:date><SPAN=20 style=3D"FONT-SIZE: 24pt"><o:p></o:p> Summary:<o:p></o:p> The AIAA through the Applied Aerodynamics, = Aircraft=20 Design, Design Engineering and Flight Test Technical Committees and the = AIAA=20 Foundation invites all university students to participate in the = <SPAN=20 style=3D"FONT-FAMILY: Cancun">Cessna/ONR Student Design/Build/Fly=20 Competition. The = contest=20 will provide a real-world aircraft design experience for engineering = students by=20 giving them the opportunity to validate their analytic studies. Student teams will design, fabricate, and=20 demonstrate the flight capabilities of an unmanned, electric powered, = radio=20 controlled aircraft that can best meet the specified mission profile. = The goal=20 is a balanced design possessing good demonstrated flight handling = qualities and=20 practical and affordable manufacturing requirements while providing a = high=20 vehicle performance. To encourage innovation and maintain a = fresh design=20 challenge for each new year, the design requirements and performance = objectives=20 will be updated for each new contest year. The changes will provide new = design=20 requirements and opportunities, while allowing for application of = technology=20 developed by the teams from prior years. Cash prizes are $2500 = for=20 1st, $1500 for 2nd and $1000 for 3rd = place. The=20 winning teams will be invited to present their designs at the 2004 AIAA = Flight=20 Test & Evaluation conference. Judging:<o:p></o:p> Students must design, document, fabricate, = and=20 demonstrate the aircraft they determine as best capable of achieving the = highest=20 score on the specified mission profile(s). Flight scores will be based = on the=20 demonstrated mission performance obtained during the contest. Each team must also submit a written = Design Report.=20 A maximum of 100 points will be awarded for the team design report. = Scores for=20 the written reports will be announced at the beginning of the = fly-off. Each aircraft will have computed a Rated = Aircraft=20 Cost, reflecting the complexity/technology of the design. The overall team score is a combination of = the=20 Design Report, Rated Aircraft Cost and Flight scores. The team with the = highest=20 overall team score will be declared the winner. Contest = Site:<o:p></o:p> Host for the competition = will be the=20 Cessna Aircraft Company. The fly-off will be held at The Cessna Pawnee = East=20 Field at <st1:place><st1:City>Wichita</st1:City>=20 <st1:State>Kansas</st1:State></st1:place>. You can check on weather historical = conditions at=20 www.weatherbase.com or www.weatherunderground.com. Team=20 Requirements:<o:p></o:p> All team members (except for a = pre-approved=20 designated pilot) must be full time students at an accredited University = or=20 College and student members of the AIAA. The team must be composed of = both under=20 classmen and upper classmen, with at least 1/3 of the members being = under=20 classmen (Freshman, Sophomores or Juniors). The pilot must be an AMA=20 (<st1:place><st1:PlaceType>Academy</st1:PlaceType> of = <st1:PlaceName>Model=20 Aeronautics</st1:PlaceName></st1:place>) member. Teams may use a = non-university=20 member for the pilot if desired. We will also provide qualified pilots = on the=20 contest day for any teams who are unable to have their pilot attend. Past Year=20 Reports:<o:p></o:p> The top scoring report from the past years = competition will be available for reference on the contest web site. The = team=20 with the top scoring report from this years contest will be required to = submit=20 an electronic copy of their report following the competition, which will = be=20 placed on the contest web site for the next years competition. Sponsorship:<o:p></o:p> Teams may solicit and accept sponsorship = in the form=20 of funds or materials and components from commercial organizations. All = <SPAN=20 style=3D"COLOR: red">design, analysis and=20 fabrication of the contest entry is the sole = responsibility of the=20 student team members. Schedule:<o:p></o:p> A completed electronic entry form is due = to the=20 contest administrator on or before <st1:date Year=3D"2003" Day=3D"31"=20 Month=3D"10">31 October=20 2003</st1:date>. The entry form for the DBF is different = than that=20 used for all other AIAA student competitions.<SPAN=20 style=3D"mso-spacerun: yes"> The DBF entry form is a = MS-Word file and=20 can be found on the contest web site. It must be submitted by e-mail to = the=20 contest administrator at <A=20 href=3D"mailto:gregory.s.page@nrl.navy.mil">gregory.s.page@nrl.navy.mil</= A> . Be=20 sure to include the Phone and FAX number for your team advisor and at = least one=20 student contact so we may reach you in case of any last minute problems = or=20 changes. All teams are = required to=20 provide two point-of-contact e-mail addresses with their contest = application,=20 one of which must be the teams advisor. =20 <I=20 style=3D"mso-bidi-font-style: normal">It is the teams responsibility to = make sure=20 the e-mail contact addresses they supply remain active during the entire = period=20 from entry to the close of the competition, as e-mail will be the = primary means=20 to provide information and updates.<o:p></o:p> Please=20 Note: the Entry = Name may not=20 be changed once the form is submitted, but must be retained and used in = all=20 reports and correspondence during the competition year. Written reports (5=20 hard copies, electronic reports will not be accepted), = are due to=20 the contest administrator by COB <st1:date Year=3D"2004" Day=3D"9"=20 Month=3D"3">9 March = 2004</st1:date>.<SPAN=20 style=3D"mso-spacerun: yes"> Reports will be judged =93as=20 received=94, no =93corrections/additions/page = changes=94 will=20 be made by the organizers so check your reports carefully before sending = them. COB is taken as = <st1:time=20 Hour=3D"17" Minute=3D"0">5 pm</st1:time> local time at the address = provided for=20 delivery of the written reports. = Scores for the written reports will be announced at the beginning = of the=20 fly-off. (A note=20 primarily for foreign entrants but also allowed for domestic teams. If sending the report by = courier is=20 prohibitive you may send it electronically to a commercial = printer (<SPAN=20 class=3DSpellE>KINKO=92s comes to mind) local to the report = submission=20 address and have them print/collate and DELIVER the reports to meet the=20 deadline. No deadline = exceptions=20 will be made, but this may be easier than international courier=20 service.)<o:p></o:p> The contest is scheduled for <SPAN=20 style=3D"COLOR: red">23-25 April 2004.<SPAN=20 style=3D"mso-spacerun: yes"> The competition will run from = <st1:time=20 Hour=3D"12" Minute=3D"0">noon</st1:time> to <st1:time Hour=3D"17"=20 Minute=3D"0">5PM</st1:time> on Friday, and <st1:time Hour=3D"8" = Minute=3D"0">8AM to=20 5PM</st1:time> on Saturday and Sunday. Final awards will be presented at = the end=20 of Sunday's competition. All teams are encouraged to stay and attend the = awards=20 presentations on Sunday. Please note that tech inspections will be = available=20 on Friday 23 April. Teams are = encouraged=20 to be prepared to have your plane inspected on Friday. Inspections will = also be=20 available on Saturday, but waiting until Saturday to go through tech may = mean=20 that your team will miss one or more rounds through the flight queue. If = we have=20 a full turnout you may not be able to get in a full set of scoring = flights=20 unless you are "ready to fly" at every opportunity. Late entries will <SPAN=20 style=3D"COLOR: red">NOT be accepted.<SPAN=20 style=3D"mso-spacerun: yes"> Late or incomplete report = submissions=20 will NOT be judged. Teams who = do not=20 submit the required written reports will NOT be=20 allowed to fly. It is the = teams=20 responsibility to assure that all deadlines are met, as they will be = <SPAN=20 style=3D"COLOR: red">strictly enforced. Communications:<o:p></o:p> The contest administration will maintain a = World=20 Wide Web site containing the latest information regarding the contest = schedules,=20 rules, and participating teams. The contest web site will also contain a = list of=20 potential suppliers for materials and equipment available to build an = entry. The=20 contest web site is located at: <SPAN=20 style=3D"COLOR: = blue">http://www.aae.uiuc.edu/aiaadbf<o:p></o:p> Later in the academic year, the website = will be=20 moved to <SPAN=20 style=3D"COLOR: blue">http://www.ae.uiuc.edu/~aiaadbf Questions regarding the contest, = schedules, or rules=20 interpretation may be sent to the contest administrator by e-mail = at: <SPAN=20 style=3D"COLOR: blue">gregory.s.page@nrl.navy.mil<o:p></o:p> The contest administrator will provide = e-mail copies=20 of questions received and their answers to all teams of record. Written reports (only) should be sent to = the chief=20 of scoring at: AIAA = Design/Build/Fly=20 Contest/Report Judging Kelly Laflin Cessna=20 Aircraft Company Dept. 363 P Cessna Aircraft Company 5800 = East Pawnee=20 Wichita, KS 67218 316-831-2247<o:p></o:p> Aircraft Requirements -=20 General<o:p></o:p> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">The=20 aircraft may be of any configuration except rotary wing or = lighter-than-air.=20 <LI class=3DMsoNormal=20 style=3D"COLOR: black; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto; mso-list: l11 level2 lfo3; tab-stops: list = 1.0in"><SPAN=20 style=3D"COLOR: windowtext">No payload may be carried internal to = the wing=20 proper. Payload in the "fuselage" may be carried in the area where = the wing=20 carry-over structure passes. For blended-wing configurations, = the=20 "fuselage" is defined to be the inner most 9=20 inch of semi-span, the remainder is "wing" for payload=20 considerations. <o:p></o:p> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Must=20 be propeller driven and electric powered with an unmodified = over-the-counter=20 model electric motor. May use multiple motors and/or propellers. May = be=20 direct drive or with gear or belt reduction.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">All=20 motors must be from the Graupner=20 or Astro Flight = families of=20 brushed electric motors, only =20 (motor should have manufacturers label visible to the judges = during=20 the technical inspection).=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">For=20 safety, each aircraft will use a commercially produced propeller. = Teams may=20 modify the propeller diameter by clipping the tip, and may paint the = blades=20 to balance the propeller. = No=20 other modifications to the propeller are allowed.<SPAN=20 style=3D"mso-spacerun: yes"> Commercial ducted fan = units are=20 allowed.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Motors=20 and batteries will be limited to a maximum of 40 Amp current draw by = means=20 of a 40 Amp fuse (per motor or pack) in the line from the positive = battery=20 terminal to the motor controller. Only ATO or blade style plastic = fuses may=20 be used. ("Maxi" size Slow Blow, 1.15"x0.85". Available online=20 www.Mcmaster.com part #7460K51 $1.66 each)=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Must=20 use over the counter NiCad batteries. = For safety,=20 battery packs must have shrink-wrap or other protection over all = electrical=20 contact points. The individual cells must be commercially available, = and the=20 manufacturers label must be readable (i.e. clear shrink wrap = preferred). All=20 battery disconnects must be "fully insulated" style connectors.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Maximum=20 battery pack weight is 5 lb. <st1:place>Battery</st1:place> pack = must power=20 propulsion and payload systems only. Radio Rx and servos MUST = be on a=20 separate battery pack. Batteries may not be changed or charged = between=20 sorties during a flight period.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Aircraft=20 and pilot must be AMA legal. This means that the aircraft TOGW = (take-off=20 gross weight with payload) must be less than 55 lb, and the = pilot must=20 be a member of the AMA.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l11 level2 lfo3; tab-stops: list 1.0in">Since=20 this is an AMA sanctioned event, the team must submit proof that the = aircraft has been flown prior to the contest date (in flight photo) = to the=20 technical inspection team. Contest supplied qualified pilots will be = available to teams who require them.=20 <LI class=3DMsoNormal=20 style=3D"COLOR: red; mso-margin-top-alt: auto; = mso-margin-bottom-alt: auto; mso-list: l11 level2 lfo3; tab-stops: list = 1.0in">Teams=20 will present a completed a signed (by the teams faculty advisor) = copy of=20 their Rated Aircraft Cost worksheet to the judges during technical=20 inspection for verification. The Rated Aircraft Cost assigned at the = technical inspection will be used for the competition and may not be = modified during the event. <o:p></o:p></LI></UL></UL> Aircraft Requirements -=20 Safety<o:p></o:p> All vehicles will undergo a safety = inspection by a=20 designated contest safety inspector prior to being allowed to make any=20 competition or non-competition (i.e. practice) flight. All decisions of = the=20 safety inspector are final. Safety inspections will include the = following as a=20 minimum. <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l1 level2 lfo6; tab-stops: list 1.0in">Physical=20 inspection of vehicle to insure structural integrity. = </LI></UL></UL> <OL type=3D1> <OL type=3D1> <OL type=3D1> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 all components adequately secured to vehicle. Verify all fasteners = tight=20 and have either safety wire, locktite = (fluid) or=20 nylock nuts.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 propeller structural and attachment integrity.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Visual=20 inspection of all electronic wiring to assure adequate wire gauges = and=20 connectors in use. Teams must notify inspector of expected maximum = current=20 draw for the propulsion system.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Radio=20 range check, motor off and motor on.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Verify=20 all controls move in the proper sense.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l10 level3 lfo9; tab-stops: list 1.5in">Check=20 general integrity of the payload system. </LI></OL></OL></OL> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l7 level2 lfo12; tab-stops: list 1.0in">Structural=20 verification. All aircraft will be lifted with one lift point at = each wing=20 tip to verify adequate wing strength (this is "roughly" equivalent = to a 2.5g=20 load case) and to check for vehicle cg location. <SPAN=20 style=3D"COLOR: red">Both upright and inverted wing lift tests will = be=20 performed. = Teams must=20 mark the expected empty and loaded cg locations on the exterior of = the=20 aircraft fuselage. Special provisions will be made at the time of = the=20 contest for aircraft whose cg does not fall within the wing tip = chord. This=20 test will be made with the aircraft filled to its maximum = payload=20 capacity.=20 <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l7 level2 lfo12; tab-stops: list 1.0in">Radio=20 fail-safe check. All aircraft radios must have a fail-safe mode that = is=20 automatically selected during loss of transmit signal. The fail-safe = will be=20 demonstrated on the ground by switching off the transmit radio. = During fail=20 safe the aircraft receiver must select: </LI></UL></UL> Throttle closed Full up elevator = Full=20 right rudder Full right (or left) aileron Full Flaps down (if so = equipped) During Fail = Safe the=20 payload release system must NOT activate.<o:p></o:p> The radio Fail Safe provisions = will be=20 strictly enforced.<o:p></o:p> <UL type=3Ddisc> <UL type=3Dcircle> <LI class=3DMsoNormal=20 style=3D"mso-margin-top-alt: auto; mso-margin-bottom-alt: auto; = mso-list: l8 level2 lfo15; tab-stops: list 1.0in">All=20 aircraft must have a mechanical motor arming system separate from = the=20 onboard radio Rx switch. This MUST = be the=20 contest specified "blade" style fuse. This device must be located so = it is=20 accessible by a crewmember standing ahead of the = propeller(s)=20 for pusher aircraft, and standing behind the = propeller(s) for=20 tractor aircraft (i.e. the crew member must not reach across the = propeller=20 plane to access the fuse). The "Safety Arming Device" will be in = "Safe" mode=20 for all payload changes. The aircraft Rx should always be powered on = and the=20 throttle verified to be "closed" before activating the motor arming=20 switch. Fuses MUST be = accessible from outside the aircraft and act as the "<SPAN=20 class=3DSpellE>safeing" device. </LI></UL></UL> <st1:place><SPAN=20 style=3D"FONT-SIZE: 13.5pt">Mission</st1:place><SPAN=20 style=3D"FONT-SIZE: 13.5pt"> Profile:<o:p></o:p> Teams must complete the flight missions as = outlined=20 in the mission matrix below. = Teams=20 will have a maximum of <SPAN=20 style=3D"FONT-SIZE: 14pt; mso-bidi-font-size: 12.0pt">5 = flight=20 attempts. A flight attempt is defined as advancing the throttle = =93stick=94 for=20 take-off. The best Single Flight Score from each of = 2=20 different mission types will be summed for the team's = Total Flight=20 Score. In the event that, due to time or = facility=20 limitations, it is not possible to allow all teams to have the maximum = number of=20 flight attempts, the contest committee reserves the right to ration = and/or=20 schedule flights. The exact determination of how to ration flights will = be made=20 on the contest day based on the number of entries, weather, and field=20 conditions.<o:p></o:p> Each team's overall score will be computed = from=20 their Written Report Score, Total Flight Score, and = the=20 Rated Aircraft Cost using the formula: SCORE =3D Written = Report Score *=20 Total Flight Score Rated Aircraft Cost<o:p></o:p> <A=20 name=3DOLE_LINK1></A><st1:place><SPAN=20 style=3D"FONT-SIZE: 18pt">Mission</st1:place><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> = Task=20 Matrix<o:p></o:p> <DIV align=3Dcenter> <TABLE class=3DMsoNormalTable=20 style=3D"WIDTH: 5.25in; mso-cellspacing: .6pt; mso-padding-alt: 5.4pt = 5.4pt 5.4pt 5.4pt"=20 cellSpacing=3D1 cellPadding=3D0 width=3D630 border=3D1> <TBODY> <TR style=3D"mso-yfti-irow: 0"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: = OLE_LINK1"><st1:City><st1:place><SPAN=20 style=3D"mso-bookmark: = OLE_LINK1">Mission</st1:place></st1:City><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Description</TD></TR> <TR style=3D"mso-yfti-irow: 1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> </TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">General Mission=20 Information<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must fit in a 2-ft wide by = 1-ft=20 high by 4-ft long (interior dimensions) box.<SPAN=20 style=3D"mso-spacerun: yes"> Note: The aircraft does = not need=20 to =93fold=94 to fit in the box, but may employ =93plug-in=94 = joints for rapid=20 assembly/disassembly. = All=20 electrical connections should be keyed so they cannot be=20 misassembled. Tape = may be=20 used as a non-structural =93latch=94 to hold components in place, = such as=20 taping a wing joint when using a plug-in spar arrangement to keep = the wing=20 from sliding loose. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Teams must select one of the = following=20 missions for each flight. =20 Teams may select a different mission for each of their = scoring=20 flight attempts. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Take-off distance is 150 ft wheels = off the=20 runway. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On landing the aircraft must land = on the=20 runway (but may roll off) to obtain a score for that = flight. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>All payloads must be adequately = secured=20 using mechanical means. = Tape=20 and Velcro are not acceptable forms of restraint. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum mission time is = <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><SPAN=20 style=3D"FONT-SIZE: 14pt; mso-bidi-font-size: = 12.0pt">10=20 minutes.</TD></TR> <TR style=3D"mso-yfti-irow: 2"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Fire = Fight<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Heavy=20 Lift/Slow Flight<o:p></o:p></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Fire Bomber DF =3D=20 2.0<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft will begin the mission = time=20 empty. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The flight mission will consist of = two=20 sorties. (1) Aircraft will be loaded, take-off, dump its water = load=20 during the downwind leg, and return to land. (2) Aircraft will = be=20 reloaded, take-off, dump its water load during the downwind leg, = and=20 return to land. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum allowed aircraft water = capacity is=20 4 liters. <I=20 style=3D"mso-bidi-font-style: normal">(Aircraft=20 will be emptied then filled to overflow during the tech = inspection.<SPAN=20 style=3D"mso-spacerun: yes"> Total volume must be 4 = liters or=20 less.) <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Teams will load the aircraft during = the=20 mission from four 2-liter plastic =93soda=94 bottles.<SPAN=20 style=3D"mso-spacerun: yes"> Teams may use gravity = loading or=20 =93pumped=94 loading. = Soda=20 bottles may NOT be pressurized to assist loading. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On all laps flown the aircraft must = complete a single 360o turn in the direction = opposite of=20 the base and final turns on the downwind leg of each lap. = <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Water may only be dumped during the = downwind leg between the upwind and downwind turn = markers/flags.<SPAN=20 style=3D"mso-spacerun: yes"> <I=20 style=3D"mso-bidi-font-style: normal">Aircraft must fly slow = enough to allow=20 sufficient time for the water to be emptied. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum dump orifice diameter is = 0.5 inch.=20 (Measured at the = exit so it=20 may be easily verified during the tech inspection). <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The pilot must call =93Dump = On=94 and=20 =93Dump Off=94 so the observer judge can easily verify that the = water dump is=20 restricted to the downwind leg. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"COLOR: red; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Early or = Late=20 water dumping, including inadvertent release of water during a = hard=20 landing, will incur a 3-min time penalty per = occurrence. Excessive=20 water spillage during loading will incur a 1-min time penalty per=20 infraction. The = flight line=20 judge will notify the team of the penalty at the time of the=20 infraction. Gross = and/or=20 deliberate spillage will disqualify the flight but will count as = one of=20 the teams=92 flight attempts. A 3-min time penalty will be = added if=20 the aircraft is not empty on landing after the final=20 lap.<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>A time penalty of 3 minutes will be = added=20 for an incomplete second lap. =20 If the second lap is not attempted or the 360o = turn is=20 not completed the second lap will be timed as = =93incomplete.=94 <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The weight of the water will be = determined=20 by the starting and ending weight of the team=92s ground-based = storage=20 =93tanks,=94 taken when entering and leaving the flight = box. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]><B=20 style=3D"mso-bidi-font-weight: normal">Single Flight Score = is: DF=20 * Lbs_Water / <SPAN=20 class=3DSpellE>Mission_Time</TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"></TR> <TR style=3D"mso-yfti-irow: 3; mso-yfti-lastrow: yes"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 23.88%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"23%"> <SPAN=20 style=3D"mso-bookmark: = OLE_LINK1">Ferry<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">High Speed=20 Flight<o:p></o:p></TD><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 75.64%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"75%"> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1">Ferry DF =3D=20 1.0<o:p></o:p> <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must take-off, complete = four laps,=20 and land. The = aircraft will=20 have no water payload for this flight <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>On all laps flown the aircraft must = complete a 360o turn in the direction opposite of the = base and=20 final turns on the downwind leg of each lap. <SPAN=20 style=3D"mso-bookmark: OLE_LINK1"><![if !supportLists]><SPAN=20 style=3D"FONT-FAMILY: Symbol; mso-fareast-font-family: Symbol; = mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]><B=20 style=3D"mso-bidi-font-weight: normal">Single Flight Score = is: DF=20 / Mission_time</TD><SPAN=20 style=3D"mso-bookmark: = OLE_LINK1"></TR></TBODY></TABLE></DIV><SPAN=20 style=3D"mso-bookmark: OLE_LINK1"> "Mission Flight Time" is the time from = when the=20 official calls "go" until the aircraft comes to a <SPAN=20 style=3D"COLOR: red">complete stop <B=20 style=3D"mso-bidi-font-weight: normal"><SPAN=20 style=3D"COLOR: red">PAST the starting line at the = completion of=20 all laps. Aircraft that = run off the=20 runway before reaching the start line may be carried to the line to end = the=20 time. Aircraft that are = damaged may=20 NOT be carried to the line to end the time, but will instead have the = time end=20 where the aircraft stops with the last lap scored as = =93incomplete.=94 For aircraft not completing the full = number of laps=20 specified for a mission, a penalty of 3 minutes will be added to the = aircraft's=20 measured "Total Mission Time" = for=20 each lap not = completed.<SPAN=20 style=3D"mso-spacerun: yes"> For example, if an aircraft = completes=20 only 3 laps of a 4 lap mission in 5 minutes, the "Total Mission Time" = would be:=20 5 minutes + 1 incomplete laps @ 3 minutes each =3D 8 minutes. <SPAN=20 style=3D"FONT-SIZE: 18pt">Aircraft Cost Model<o:p></o:p> Rated = Aircraft=20 Cost, $ (Thousands) =3D (A*MEW + B*REP + C*MFHR)/1000 <DIV align=3Dcenter> <TABLE class=3DMsoNormalTable=20 style=3D"WIDTH: 409.8pt; mso-cellspacing: .6pt; mso-padding-alt: 5.4pt = 5.4pt 5.4pt 5.4pt"=20 cellSpacing=3D1 cellPadding=3D0 width=3D683 border=3D1> <TBODY> <TR style=3D"mso-yfti-irow: 0"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> <SPAN=20 class=3DSpellE>Coef.</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Description</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Value</TD></TR> <TR style=3D"mso-yfti-irow: 1"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> A</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturers Empty Weight Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $300 <SPAN=20 style=3D"COLOR: red">(NEW)<o:p></o:p></TD></TR> <TR style=3D"mso-yfti-irow: 2"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> B</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Rated Engine Power Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $1500</TD></TR> <TR style=3D"mso-yfti-irow: 3"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> C</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturing Cost Multiplier</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> $20 / hour</TD></TR> <TR style=3D"mso-yfti-irow: 4"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> MEW</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturers Empty Weight</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Actual airframe weight [lb] with all=20 flight and propulsion batteries but without any = payload.</TD></TR> <TR style=3D"mso-yfti-irow: 5"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> REP</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Rated Engine Power</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> (1+.25*(# engines-1)) * Total=20 <st1:place>Battery</st1:place> Weight=20 [lbs]<o:p></o:p> "Total = <st1:place>Battery</st1:place>=20 Weight" will be the weight of the propulsion battery = pack(s) as=20 determined by the judges scale during = technical=20 inspection. Total propulsion battery pack weight may not exceed 5 = lb, but=20 it may be lighter.</TD></TR> <TR style=3D"mso-yfti-irow: 6; mso-yfti-lastrow: yes"> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 11%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"11%"> MFHR</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Manufacturing Man Hours</TD> <TD=20 style=3D"PADDING-RIGHT: 5.4pt; PADDING-LEFT: 5.4pt; PADDING-BOTTOM: = 5.4pt; WIDTH: 44%; PADDING-TOP: 5.4pt"=20 vAlign=3Dtop width=3D"44%"> Prescribed assembly hours by WBS (Work Breakdown = Structure). MFHR =3D S WBS = hours WBS 1.0=20 Wing(s): = (NEW)<o:p></o:p> 10 hr/ft^2 Wing Span * Chord * # wings Wing Span is = longest=20 distance perpendicular to fuselage axis on any wing.<SPAN=20 style=3D"mso-spacerun: yes"> Chord is maximum exposed = wing=20 chord on any wing. = For a=20 blended wing-body, exposed wing starts 9 inch out from the body=20 centerline. 5 hr * <SPAN=20 class=3DSpellE>control_function_multiplier ailerons =3D = 1 <SPAN=20 class=3DSpellE>flaperons =3D 1.5 ailerons + flaps =3D = 2 ailerons +=20 spoilers =3D 2 ailerons + flaps + spoilers =3D 3 WBS 2.0 = Fuselage=20 (NEW)<o:p></o:p> 20 hr/ft^3 Body Length x Width x Height Length is = maximum=20 body length. Width = is maximum=20 body width. Height = is maximum=20 body height (does not include landing gear height).<SPAN=20 style=3D"mso-spacerun: yes"> Maximum body width and = maximum=20 body height may occur at different fuselage locations. For = a=20 blended wing-body, body width is fixed at 18 inch. Note: = Maximum=20 length of the body is defined to be the longest longitudinal = length=20 possible to measure on the aircraft, and may include spinner and = part of=20 vertical or horizontal surfaces. WBS 3.0=20 Empennage<o:p></o:p> 5 hr/Vertical Surface (Any vertical surface, including = winglets,=20 struts, end plates, ventral etc) with no active control 10=20 hr/Vertical Surface (Any vertical surface) with an active=20 control 10 hr/Horizontal Surface. A horizontal surface is a = "wing"=20 if it is more than 25% of the span of the greatest span horizontal = surface.) A "V" tail is considered to be a Vertical surface without = control (5=20 hr) plus a horizontal surface with controls (10 hr), for a total = of 15=20 hr. WBS 4.0 = Flight=20 Systems<o:p></o:p> 5 hr/servo or motor controller WBS 5.0 = <SPAN=20 style=3D"COLOR: red">(Deleted)<o:p></o:p> </TD></TR></TBODY></TABLE></DIV> <o:p></o:p> Rated Aircraft Cost must be = supplied=20 when the aircraft enters the technical inspection. The RAC worksheet = must be=20 signed by the team advisor. RAC may = not be=20 changed during the competition unless it is determined by the contest = officials=20 to be inaccurate or inappropriate. The contest officials reserve the = right to=20 audit and revise the RAC for omissions or errors at any time. <SPAN=20 style=3D"FONT-SIZE: 18pt">General Mission Specification and=20 Notes:<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft are to remain assembled while = waiting in=20 the queue. Teams will = install the=20 propulsion batteries once reaching the <B=20 style=3D"mso-bidi-font-weight: normal">3rd =93On=20 Deck=94 position (i.e. when the aircraft is 3rd in = the=20 queue, the team must begin to install the batteries). <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft may = not=20 have any work performed in the starting line queue, other than as = specified=20 above at the 3rd On Deck position. Aircraft propulsion = batteries may=20 be left out of the aircraft when in line. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft batteries may be charged while = the=20 aircraft is in the queue IF AND ONLY = IF the=20 batteries are removed from the aircraft. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The aircraft propulsion system(s) must be = disarmed or "safed" during any time when = crew members=20 are preparing the aircraft. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Maximum flight support crew is: pilot, = observer,=20 and 3 ground crew. Only the designated ground crew may reload the = aircraft=20 payload . Pilot and observer may be members of the ground crew, provided = total=20 ground crew size remains 3 people. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Observer and all ground crew must be=20 students. <SPAN=20 style=3D"COLOR: red">Only the pilot may be a non-student. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>The upwind turn will be made after = passing the=20 upwind pylon. The downwind turn will be made after passing the downwind = pylon.=20 Upwind and downwind pylons will be 500 ft from the starting line. = Aircraft must=20 be "straight and level" when passing the pylon before initiating the = turn. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must land on the paved portion = of the=20 runway. Aircraft may "run-off" the runway during roll-out. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>After landing, aircraft <SPAN=20 style=3D"COLOR: red">may taxi back to the starting line. = Alternatively,=20 aircraft may be carried back to the starting line; however, the team may = not=20 leave the pit area to retrieve the aircraft until the aircraft has come = to a=20 complete stop, and they are signaled it is "Ok" to retrieve the aircraft = by the=20 flight line judge. <I=20 style=3D"mso-bidi-font-style: normal">Aircraft experiencing damage = during landing=20 will be considered to have completed their flight where they come to = rest and my=20 not be =93carried=94 to the starting line to =93complete=94 a = lap. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft will be considered to have only = minor=20 damage if they can be repaired and presented as flight worthy within = 30=20 minutes of the end of that flight period. Aircraft with only minor = damage=20 will be credited with their full Single Flight Score. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft that can be repaired during the=20 competition, but not within 30 minutes of the flight period, will NOT be = credited with a score for that flight period. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Flight altitude must be sufficient for = safe=20 terrain clearance and low enough to maintain good visual contact with = the=20 aircraft. Decisions on safe flight altitude will be at the discretion of = the=20 flight line judges and all rulings will be final. Additional information is included in the = <A=20 href=3D"http://www.ae.uiuc.edu/2003%20DBF/2003_faq.html">FAQ</A> = (Frequently Asked=20 Questions). Protest=20 Procedures<o:p></o:p> Submitting a protest against a competing = team is a=20 serious matter and will be treated as such. Teams may submit a protest = to the=20 Contest Administrator at any time during the competition. Protests must = be=20 submitted in writing and signed by the team advisor (if present at the=20 competition) or the team captain if a faculty advisor is not present. = Protests=20 will be posted for all teams to review. If the protest is rejected, the submitting = team(s)=20 will forfeit one of their remaining flight attempts. If all flight = attempts have=20 been used, the team(s) will forfeit their lowest Single Flight = score. Protests and the appropriate penalty = (ranging from a=20 requirement to repeat a flight for minor infractions to disqualification = from=20 the contest for deliberate attempts to misinform officials or violate = the=20 contest rules) will be decided by the Contest Administrator and the = Contest=20 Director, in consultation with other Contest Officials. The decision of = the=20 Contest Administrator and Contest Director is final. NEW<SPAN=20 style=3D"FONT-SIZE: 13.5pt"> for This Year<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Inverted wing tip lift test was added <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft missions are revised. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Missions have different difficulty = factors=20 applied. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>Aircraft must fit in a specified size = shipping=20 container, but assembly time is NOT part of the mission scoring. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>RAC formulas have been rescaled. <![if !supportLists]><SPAN=20 style=3D"FONT-SIZE: 10pt; FONT-FAMILY: Symbol; mso-fareast-font-family: = Symbol; mso-bidi-font-size: 12.0pt; mso-bidi-font-family: Symbol"><SPAN=20 style=3D"mso-list: Ignore">=B7<SPAN=20 style=3D"FONT: 7pt 'Times New = Roman'"> =20 <![endif]>3-view drawing in report must be = on an 11=20 x 17 inch page for easier reading by judges Design = Report:<o:p></o:p> Each team will submit a judged design = report as=20 outlined below. The submission date is contained in the schedule section = of this=20 document. Reports must be bound. (Simple spiral bindings are sufficient = and=20 preferred; 3-ring binders are not allowed.) All information used for = scoring=20 must be in the outlined sections. Reports exceeding the total page = limit will=20 be scored as "1 of 100". Appendices may not be included. All reports will be space and one half, = 10-pt Arial=20 font. Tables and figures will also be 10-pt Arial font. Margins are 1 = inch on=20 all sides. Report pages will be 8 1/2 x 11 inch with the exception of = the=20 drawing package. The = drawing=20 package may be 11 x 17 inch pages. =20 The 3-view drawing must be on = an 11 x 17=20 inch page. Absolute maximum page count for the report = is=20 60 pages, including text, = tables, and=20 figures (cover/title page and table of contents is extra). Drawing = package may=20 not comprise more than 5 of the pages of the report page limit. All figures must be either half (1/2) page = or full=20 (1) page format. No exceptions. Please note that the judges will be = using this=20 same report outline for evaluating reports. ALL items listed will = be=20 expected to be present, easy to locate and identify and well documented = in the=20 report for a maximum score.<o:p></o:p> <SPAN=20 style=3D"FONT-SIZE: 16pt; mso-bidi-font-size: 13.5pt">Design=20 Report<o:p></o:p> <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">1.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Executive Summary: (5 points): Provide a = summary of=20 the development of your design. This should be a narrative description=20 highlighting the major areas in the development process for your final=20 configuration and a broad description of the range of design = alternatives=20 investigated. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">2.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Management Summary (5 points): Describe the=20 organization of the design team. Provide a chart of design personnel and = assignment areas. Include a (single) milestone chart showing planned and = actual=20 timing of major elements of the design process, including as a minimum = the=20 conceptual design stage, preliminary design stage, detailed design = stage, flight=20 testing and report preparation periods. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">3.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Conceptual Design (20 points): Describe the = key=20 elements of the mission requirements (problem statement).<SPAN=20 style=3D"mso-spacerun: yes"> Document the alternative = configuration=20 concepts (e.g. biplane, canard, flying wing, pusher -Vs tractor, number = of=20 engines etc.) investigated during the conceptual design stage and the = reason why=20 each concept was considered. Describe and document the numerical figures = of=20 merit (FOM's) used to screen competing = concepts, and=20 the mission feature each FOM was selected to support. Rated = Aircraft=20 Cost should be one of the FOM=92s<SPAN=20 style=3D"mso-spacerun: yes"> used during the screening = process.<SPAN=20 style=3D"mso-spacerun: yes"> Numerical data need not be = extensive at=20 this stage, but should include as a minimum: a final ranking chart = giving the=20 quantitative value of each design for each FOM. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">4.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Preliminary Design (30 points): Document the = design=20 parameter and sizing trades investigated during the preliminary design = stage,=20 and why each was felt to be important to the mission. Describe the = analysis=20 methods used. Describe the mission model used and the predicted = performance.=20 Provide estimates of the aircraft lift, drag and stability = characteristics.<SPAN=20 style=3D"mso-spacerun: yes"> Document the design = optimization and=20 trade studies conducted and their results. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">5.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Detail Design (15 points for discussion items, = 10 points=20 for drawing package, 25 points total for the section): Document = component=20 selection and systems architecture selection. Include your final = competition=20 aircraft's Rated Aircraft Cost using the contest supplied = cost=20 model. RAC table should = include all=20 input parameter, intermediate and final computation. Include a = table=20 giving data for the sized aircraft. =20 A copy of this table must be posted by the team at their = =93pit=94 area=20 (poster board). The table = should=20 include; Geometry: length, span, height, wing area, Aspect Ratio, = control=20 volumes Performance: CL max, L/D max, maximum Rate of Climb, stall = speed,=20 maximum speed, take-off field length (two sets, empty and gross=20 weight) Weight Statement (airframe, propulsion system, control = system,=20 payload system, payload, empty weight, gross weight) Systems (radio = used,=20 servos used, battery configuration used, motor used, propeller = (nominal), gear=20 ratio (if used) The Drawing = Package will=20 be included with this section and must contain as a = minimum a=20 3-view drawing of the design in sufficient detail to indicate aircraft = size and=20 configuration; primary structure component size and location; payload = size,=20 location and restraint method; and location of propulsion and flight = control=20 system components. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">6.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Manufacturing Plan and processes (10=20 points): Document the process selected for manufacture of major = components=20 and assemblies of the final design. Detail the manufacturing processes=20 investigated, and describe the FOM's used = (including=20 but not limited to: availability, required skill levels and cost) to = screen=20 competing concepts. Describe the analytic methods (cost, skill matrix,=20 scheduling time lines) used to select the final set of manufacturing = processes.=20 Include a manufacturing milestone chart showing scheduled event = timings. <![if !supportLists]><SPAN=20 style=3D"mso-list: Ignore">7.<SPAN=20 style=3D"FONT: 7pt 'Times New Roman'"> = <![endif]>Testing Plan (5 points): Detail testing = objectives,=20 schedules, check-lists, results and any lessons learned for component = and full=20 aircraft testing, both static and dynamic (ie. in=20 flight). <IMG id=3D_x0000_i1026 = height=3D299=20 src=3D"http://www.ae.uiuc.edu/aiaadbf/images/98course.gif" width=3D480 = border=3D0> <DIV class=3DMsoNormal style=3D"TEXT-ALIGN: center" align=3Dcenter> <HR align=3Dcenter width=3D"100%" SIZE=3D3> </DIV> [<A=20 href=3D"http://www.ae.uiuc.edu/aiaadbf/2004_rules.html#top">Top</A>] [<A = href=3D"http://www.ae.uiuc.edu/aiaadbf/index.html">AIAA Student = Design/Build/Fly=20 Competition homepage</A>] [<A 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