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Studies related to the development of a multiple start-stop solid propellant rocket motorMultiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
Document ID
19670028461
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Paulson, R. A. (M.S. THESIS)
Date Acquired
August 3, 2013
Publication Date
May 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72313
Report Number: NASA-CR-72313
Accession Number
67N37790
Funding Number(s)
CONTRACT_GRANT: NAS3-2554
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SOLID PROPELLANT ROCKET ENGINE
STARTER
STOPPING POWER
AMMONIUM PERCHLORATE

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