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Development Requirements for Integrated Aircraft Power Systems
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English
Abstract
Future military aircraft will demand greater operational capability from lighter weight and more durable power systems. The historical development approach has been inadequate in assessing the needs and providing the necessary early power systems installation coordination. An expanded power systems development program can provide tangible benefits by development of system specific component technology and by providing the opportunity to improve component and system maturity prior to production release. The process can result in lighter weight systems with reduced fly-away costs and in lower costs of operation, which will more than pay for the expanded power systems development program.
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Authors
Citation
Mitnik, S. and Norman, L., "Development Requirements for Integrated Aircraft Power Systems," SAE Technical Paper 801149, 1980, https://doi.org/10.4271/801149.Also In
References
- Rhoden J. A. Scheer L. E. “Power System Study, Advanced Fighter/Attack and V/STOL Airplanes.” NAPC Final Report 41-1906 Dec. 1977
- Rhoden J. A. Wood R. R. Jethon O. “Results of Power Systems Study of Advanced Fighter/Attack and V/STOL Airplanes.” American Chemical Society 799285 1979
- Duane J. T. “Learning Curve Approach to Reliability Monitoring.” IEEE Transactions on Aerospace 2 2 April 1964