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Exploring in aerospace rocketry. 6 - Solid-propellant rocket systemsSolid propellant rocket systems design and combustion efficiency and burning rate of solid propellants
Document ID
19680010362
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mc Bride, J. F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52393
Report Number: NASA-TM-X-52393
Meeting Information
Meeting: LEWIS AEROSPACE EXPLORERS
Location: CLEVELAND
Start Date: January 1, 1966
End Date: December 31, 1967
Accession Number
68N19831
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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