Vendetta Final Proposal Part 1 (3.4 MB) - Cal Poly

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Weight BuildupComponent Weight Fuselage Butt PlaneStation (ft)(ft)StructuresWaterLine (ft)Wx(lb-ft)Wy(lb-ft)Wz(lb-ft)Wing Group 8,779 66.0 0.0 -3.0 579,319 0 -26,511Horizontal Tail 1,262 94.3 0.0 -3.0 119,073 0 -3,812Vertical Tail 1,279 86.2 0.0 -7.1 110,176 0 -9,117Fuselage 10,540 44.2 0.0 -2.1 465,770 0 -22,345Main Gear 2,289 68.9 0.0 -1.9 157,648 0 -4,371Nose Gear 400 17.3 0.0 4.7 6,915 0 1,87524,548 58.6 0.0 -2.6 1,438,902 0 -64,282PropulsionEngines 11,034 84.9 0.0 -2.7 937,198 0 -29,791Engine Mounts 138 84.9 0.0 -2.7 11,752 0 -374Firewall 102 84.9 0.0 -2.7 8,638 0 -275Nozzle 140 84.9 0.0 -2.7 11,892 0 -378Oil Cooling 77 84.9 0.0 -2.7 6,528 0 -208Starter 185 84.9 0.0 -2.7 15,679 0 -498SystemsPressurization11,67537284.917.30.00.0-2.7-4.0991,6876,43300-31,523-9,395Air Induction 2,325 64.4 0.0 -3.2 149,738 0 -788Anti-Ice 248 17.3 0.0 -4.0 4,289 0 -1,414APU 350 80.9 0.0 -4.3 28,326 0 -2,509Auxillary Gear 578 17.3 0.0 -4.0 10,005 0 -4,531Avionics 1,122 17.3 0.0 -4.0 19,416 0 -1,923C.G. Control System 476 44.2 0.0 -2.1 21,037 0 -2,917Electrical 1,376 44.2 0.0 -2.1 60,811 0 -137Engine Controls 65 84.9 0.0 -2.7 5,507 0 -10,130Flight Controls 3,752 17.3 0.0 -4.0 64,945 0 -2,492Fuel System 5,101 58.3 0.0 -2.1 297,236 0 -10,934Furnishings/Equipment 617 17.3 0.0 -4.0 10,675 0 -10,100Launchers & Weapons 2,500 55.3 0.0 -1.8 138,300 0 -1,965Hydraulic System 1,110 44.2 0.0 -2.1 49,052 0 -60Oxygen System 28 17.3 0.0 -4.0 486 0 -2,242Paint 555 44.2 0.0 -2.1 24,526 0 -43,61820,574 43.3 0.0 -5.1 890,782 0 -105,155Geometric DataItemAreasUnits Wing Horizontal VerticalReference sq. ft 1500 270 165Exposed sq. ft 900 265 160Wetted sq. ft 1714 528 330Span ft 54.8 35.1 9.2Aspect Ratio - 2.0 4.6 2.1Taper Ratio - 0.17 0.23 0.17SweepsLE ° 40 40 40c/4 ° 21 24 21c/2 ° 5 9 5TE ° -30 -30 -30ChordsMean Aerodynamic ft 32.0 14.9 10.7Root ft 46.8 15.0 16.0Tip ft 8.0 3.5 2.8BP 0.0Total Fuselage Volume: 5000.8 cubic feetFS295.6Forward FuselageBreak Point 368.4" MAC @ BP 125Wing Break PointProjected Vertical PlanformAft FuselageBreak Point178.0" MAC@ BP 11153°EMPTY 56,797 58.5 0.0 -3.5 3,321,371-200,959PayloadGBU-27 2,000 55.3 0.0 -1.8 110,640 0 -3,540GBU-272,000 55.3 0.0 -1.8 110,640 0 -3,540GBU-272,000 55.3 0.0 -1.8 110,640 0 -3,540GBU-272,000 55.3 0.0 -1.8 110,640 0 -3,540AM-120 390 55.3 0.0 -1.8 21,575 0 -690AM-120 390 55.3 0.0 -1.8 21,575 0 -690Crew & Cargo 500 55.3 0.0 -1.8 27,660 0 -8859,280 55.3 0.0 -1.8 513,370 0 -16,426054.8' (657.3")35.1' (421.8")13.5' (161.6" )20° CantFS122.7FS226.2FS275.6FS303.4FS362.8FS413.3FS551.1FS631.5FS688.9103.3' (1240.0")FS729.414°FS826.7FS964.5FS940.0128.3" MAC @ WL 101FS1051.3FS1102.3FS1175.8ZERO FUEL 66,077 58.0 0.0 -3.3 3,834,740 0 -217,38520.6'(247.5")FuelFwd. Fuselage 23,034 41.6 0.0 0 -1.9 958,460 0 -43,996Left Wing 6,366 67.0 12.9 -3.0 426,331 82,249 -19,162Right Wing 6,366 67.0 -12.9 -3.0 426,331 -82,249 -19,162Aft FuselageTAKEOFF GROSS23,20858,974125,05170.058.358.10.00.00.0-1.9-2.1-2.71,625,2333,436,3557,271,096000-44,095-126,414-323,79915.6' (187.0")F.R.L @ WL 0135°fov5.3'(63.4")VendettaChris DroneyNate Schnaible13°Kolby KeiserChris MaglioFoldout 1Aircraft OverviewChris AtkinsonDan SalluceRev. 3Scale 1:150High Rollers5/23/02
VendettaChris DroneyNate SchnaibleKolby KeiserChris MaglioFoldout 2Inboards and SectionsChris AtkinsonDan SalluceRev. 3Scale 1:150High Rollers5/23/02Retracted Main GearFull Flying StabRadar and NoseAccessoriesEngineRetracted Nose GearBP 30.0Partial Section - BP 30.0BP 0.0Forward Fuselage Tank23,034 lb JP-8Total Fuel58,974 lb JP-8Aft Fuselage Tank23,208 lb JP-8Left Wing Tank6,366 lb JP-8Tandem CockpitWeapons BayInletAPUFS295.628°30°FS122.75°FS226.2FS275.6FS303.4FS362.8FS413.3FS551.1FS631.5FS688.9FS729.4FS826.7FS964.5FS940.0FS1102.3FS1051.3FS1175.8Radar and NoseAccessoriesRetracted Main GearEngine AccessoriesFS122.7FS226.2FS275.6FS295.6FS303.4FS362.8F.R.L11°AN/APG-77IRSTAAR PortWeapons BayFlow DeflectorMPRLAPUWing Tank X 26,366 lb each70% Volume UsageNo Fuel Around Engineor Near Fan FaceForward Fuselage Tank23,034 lb JP-8BP 0.0Right Wing Tank6,366 lb JP-8Left Wing Tank6,366 lb JP-8FS413.3FS551.1FS631.5FS688.910° Fall AngleFS729.4FS826.7Aft Fuselage Tank23,208 lb JP-8Fuel Tank ContainedWithin Section BreaksForward Fuselage Tank23,034 lb80% Volume UsageAft Fuselage Tank23,208 lb80% Volume UsageTotal Fuel58,974 lb JP-8FS940.0FS964.5FS1051.3FS1102.3FS1175.8
Page 6 and 7: Figure 11.1 - 1-g Military Specific
Page 8 and 9: Nomenclature6DOF Six Degrees of Fre
Page 10: 1 IntroductionThe American Institut
Page 13 and 14: Table 1.III - Comparison of the F-1
Page 15 and 16: The weight fraction method provides
Page 17 and 18: 3 ConfigurationThe current configur
Page 19: • Span = 53 ft• m.a.c. = 32 ft
Page 23 and 24: low signature axisymmetric advanced
Page 25 and 26: 0° Lookup77°50403020100-10-20-30-
Page 27 and 28: 5.2 Wing SweepThe next wing paramet
Page 29 and 30: 5.3 Wing ThicknessThe effect of win
Page 31 and 32: 0.10.050-0.05-0.1-0.150 0.1 0.2 0.3
Page 33 and 34: 5.6 DragDrag was divided into four
Page 35 and 36: 6 PropulsionIn developing the propu
Page 37 and 38: Turbine Engine Technology (IHPTET)
Page 39 and 40: 35,00030,000Sea Level 1.5K 5K10K20K
Page 41 and 42: 0.990.980.97Pressure Recovery0.960.
Page 43 and 44: oundary layer diverter for high spe
Page 45 and 46: 7 Structural Layout & Material Sele
Page 47 and 48: Vertical AttachmentPointsHorizontal
Page 49: 8 Landing GearLanding Gear design f

Vendetta Final Proposal Part 1 (3.4 MB) - Cal Poly

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