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Abort separation including aerodynamic, dynamic, propulsive, and trajectory influencesAerodynamic effects on safe abort separation for space shuttles
Document ID
19700028514
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Decker, J. P. (NASA Langley Research Center Hampton, VA, United States)
Mc Ghee, R. J. (NASA Langley Research Center Hampton, VA, United States)
Pierpont, P. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Publication Information
Publication: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 1 JUL. 1970
Subject Category
Space Vehicles
Accession Number
70N37830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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