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Interface considerations of solid motors with RAE A, B, IMP H and J, and Pioneer F and G spacecraftInterface problems with various spacecraft which employed solid propellant rocket motors for the final propulsive stages are described along with an account of the solutions to those problems.
Document ID
19750010241
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Dembrow, D. W. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
X-470-75-43
NASA-TM-X-70853
Report Number: X-470-75-43
Report Number: NASA-TM-X-70853
Accession Number
75N18313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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