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Structural load reduction of the space shuttle booster/orbiter configuration using a load relief guidance techniqueA space shuttle booster/orbiter atmospheric ascent guidance algorithm is developed that will reduce the aerodynamically induced structural loads as compared to an open loop guidance algorithm.
Document ID
19730013085
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Deaton, A. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Kelley, P. B. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 5, 1973
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-64738
Report Number: NASA-TM-X-64738
Accession Number
73N21812
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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