A detailed preliminary design study was accomplished, and it is shown that the system is retrofitable in the existing crew stations of the A-7 and F-4 aircraft with modifications thereto. (Author)
An Investigation of an Integrated Aircrew Escape/Rescue System Capability (AERCAB)
1969
379 pages
Report
Keine Angabe
Englisch
Aircraft , Fluid Mechanics , Jet fighters , Ejection seats , Parawings , Aerospace systems , Aerodynamic characteristics , Air force research , Ejection , Stabilization , Turbofan engines , Parachutes , Navigational aids , Sequences(Mathematics) , Flight control systems , Maneuverability , Catapults , Hydraulic equipment , Homing devices , Safety belts , Survival kits , A-7 aircraft , F-4 aircraft
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