Auxiliary Power Systems for 1975 Fighter Aircraft AiResearch Manufacturing Company of Arizona, Div., Garrett Corporation

Format:

Conference/Event

Author/Creator:

Nicholls, B. H., author.

Conference Name:

National Air Transportation Meeting (1968-04-29 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1968

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

680311

Access Restriction:

Restricted for use by site license