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Flight dynamics of a straight wing space shuttle booster during entryDynamic flight control simulation for straight wing space shuttle booster entry
Document ID
19710016593
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kimbrel, L. G. (Boeing Co. Seattle, WA, United States)
Patha, J. T. (Boeing Co. Seattle, WA, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1971
Publication Information
Publication: NASA, WASHINGTON NASA SPACE SHUTTLE TECHNOL. CONF., VOL. 1 APR. 1971
Subject Category
Space Vehicles
Accession Number
71N26069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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