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SELECTED AIRCRAFT CHARACTERISTICS
APPENDIX B CANDIDATE 4 ENGINE AIRCRAFT
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100 passenger 1968 AIA METHOD 200 NM VTOL aircraft configuration aircraft designed aircraft selected AIRFRAME COST approximately attitude control AVAILABLE SEAT MILE Characteristics Summary Conceptual Design control guidelines control requirement criteria cruise engines cruise Mach number cruise speed CTOL current study DC-9 Type Empennage DESIGN CRUISE DIRECT OPERATING COST dispatch reliability engine aircraft engine configuration ETaC factors Fan Pressure Ratio fan thrust fuel fuselage gross weight GROUND EFFECT guideline changes height control HR/YR increase km/hr KTAS lb kg lead compensation mission requirements NASA nautical miles NM VTOL MISSION nozzle number of engines OPERATING COST COMPARISON parameter performance pitch reduced Remote Lift Fan reverse thrust safety SEAT km SELECTED 4 ENGINE SELECTED AIRCRAFT shown in Figure statute mile STOL takeoff and landing takeoff profile Task 1A Task IB thrust level thrust vectoring TOGW U/SEAT km updated UTILIZATION V/STOL aircraft V/STOL Lift Fan V/STOL TRANSPORT VTOGW wing yaw control