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Reaction control system augmentation for V/STOL aircraftAdvantages and problems associated with augmentation of reaction controls are discussed. The current status of compact ejector technology and the expected performance of known efficient designs for reaction control applications are presented.
Document ID
19800001891
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Streiff, H. G. (Lockheed-California Co. Burbank, CA, United States)
Donham, R. E. (Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800001868Collected WorksWorkshop on Thrust Augmenting Ejectors
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