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Structural control interactionThe basic guidance and control concepts that lead to structural control interaction and structural dynamic loads are identified. Space vehicle ascent flight load sources and the load relieving mechanism are discussed, along with the the characteristics and special problems of both present and future space vehicles including launch vehicles, orbiting vehicles, and the Space Shuttle flyback vehicle. The special dynamics and control analyses and test problems apparent at this time are summarized.
Document ID
19730013107
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ryan, R. S. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Mowery, D. K. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Winder, S. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Worley, H. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 15, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-64732
Report Number: NASA-TM-X-64732
Accession Number
73N21834
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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