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X-24B flight test programThe X-24B is an air launched, rocket powered research aircraft. A number of its design features constitute a tradeoff between aerodynamics and heating considerations. A vehicle description is given and test program objectives are discussed along with operational procedures and aspects of energy management. Attention is also given to X-24B handling qualities, approach and landing, wind tunnel data and simulation, and proposed X-24C vehicle requirements.
Document ID
19760035693
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Manke, J. A.
(NASA Flight Research Center Edwards, Calif., United States)
Love, M. V.
(USAF Edwards AFB, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76A18659
Distribution Limits
Public
Copyright
Other

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