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

Nomenclature6DOF Six Degrees of FreedomA 0i Freestream Capture Area, ft 2A 1 Inlet Capture Area, ft 2AB AfterburnerA e Area of Inlet Exit, ft 2AIAA American Institute of Aeronautics andAstronauticsAOA, α Angle-of-Attack, degAPU Auxiliary Power UnitAR Aspect RatioA s Area at Shock, ft 2b W Wing Span, ftCAS Control Augmentation SystemC D Drag CoefficientC f Friction CoefficientCG Center-of-GravityC L Wing Lift CoefficientC Lα Lift Curve SlopeC lδr Roll Moment due to Rudder DeflectionC m Pitch Moment CoefficientC mα Pitch Moment due to AOAC mδr Rudder Pitch Moment CouplingC nδr Yaw Moment due to Rudder DeflectionC yδr Side Force due to Rudder DeflectionDATCOM Air Force Data CompendiumDC Direct CurrentDFSC Digital Flight Control Systemd T Ratio of local pressure to sea-level pressureeSpan Efficiency FactorF F Form FactorGFE Government Furnished EquipmentGPS/INS Global Positioning System/InertialNavigation Systemh AltitudeHUD Heads-up-DisplayICNIA Integrated Communication, Navigation, andIdentification AvionicsIHPTET Integrated High Performance TurbineEngine TechnologyIR InfraredIRSTS Infrared Search and Track System withLaser RangingI x Moment of Inertia about the x-axis, slug-ft 2I xy Moment of Inertia in the xy plane, slug-ft 2I xz Moment of Inertia in the xz plane, slug-ft 2I y Moment of Inertia about the y-axis, slug-ft 2I yz Moment of Inertia in the yz plane, slug-ft 2I z Moment of Inertia about the z-axis, slug-ft 2k 1 Induced Drag FactorK SM Static MarginL/D Lift-to-Drag ratioviiiL/HLANTIRNLBR-TFLEL HTL VTMMMAC, c Wm eMFDMPRLNNACANATONPFNPF cOBIGGSOBOGSOEIPP sP SLqQ FQ TrRAMRATRCSReRFPRTD&ER xR yR zInlet Length to Height RatioLow-Altitude Navigation and TargetingInfraRed for NightLow-Bypass-Ratio Turbo FanLeading EdgeHorizontal Tail Arm, ftVertical Tail Arm, ftMach NumberActual Mass Flow RateMean Aerodynamic Chord, ftEstimated Mass Flow Rate, slug/sMultifunction DisplayMultipurpose Rotary LauncherLoad FactorNational Advisory Committee forAeronauticsNorth Atlantic Treaty OrganizationNet Propulsive ForceCorrected Net Propulsive ForceOn Board Inert Gas Generation SystemOn Board Oxygen Generation SystemOne Engine InoperablePressure, psfSpecific Excess Power, ft/sSea-Level Pressure, psfDynamic Pressure, psfInterference FactorRatio of local temperature to sea-levelstatic temperatureTurn Radius, ftRadar Absorbent MaterialsRam Air TurbineRadar Cross SectionReynolds NumberRequest for ProposalResearch, Test, Development, andEngineeringNon-Dimensional Radius of Gyrationabout the x-axisNon-Dimensional Radius of Gyrationabout the y-axisNon-Dimensional Radius of Gyrationabout the z-axisSurface to Air MissileSociety of Allied Weight EngineersSelf-Contained Energy Storage SystemThrust Specific Fuel Consumption,lbm/lbf-hrSAMSAWESESSFC,TSCFS HT Horizontal Tail Planform Area, ft 2S ref, S W Wing Reference Area, ft 2S VT Vertical Tail Planform Area, ft 2T Thrust, lbf