This paper defines and evaluates auxiliary power systems for a self-sufficient 1975 fighter aircraft. The mission and auxiliary power requirements for a V/STOL fighter aircraft are used as a basis for this study. Candidate systems are identified and analyzed for their take-off gross weight penalty to the aircraft for missions requiring both short-time and long-time aircraft standby periods.The components of the various systems are evaluated as to their projected efficiency, weight, and size for use in the analysis. A recommended reference system is selected as the basis for an optimized system design. Specific areas of research and development are identified as required to obtain the advanced system components.
Auxiliary Power Systems for 1975 Fighter Aircraft
Sae Technical Papers
National Air Transportation Meeting ; 1968
1968-02-01
Conference paper
English
Auxiliary power systems for 1975 fighter aircraft
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