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Figure Page 1 Design Mission Profiles
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aircraft buy aircraft cost altitude attitude control system bypass ratio control excursion control thrust cruise altitude cruise fan design cruise performance cruise speed deflection direct operating costs DOC Sensitivity DOC's duct burners engine/fan evaluation exit louver fan failure fan plus cruise fan thrust field length flight cycles fuel fuselage gas flow hot gas hover control ILF 1A1 increased inertia characteristics inlet installed integral engine integral fan integral lift fan lift cruise engines lift engines lift fan aircraft Lift Fan System lift/cruise fan maximum NASA nautical miles nominal level nominal thrust level pods Power Setting propulsion arrangement propulsion concept propulsion system reference 100 remote fan aircraft remote fan design remote fan system Remote Lift Fan scaling data segmented hood SFFAN shown in Figure slug ft.2 STOL STOL mode swingout thrust loss thrust vector thrust-to-weight ratio tip-turbine TRIP DISTANCE turbofan gas turbojet gas uninstalled V/STOL Commercial Transport VTOL wing