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Obtaining hypervelocity acceleration using propellant-lined launch tubes Progress reportStrain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with propellant lining
Document ID
19690029405
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rodenberger, C. A. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
August 5, 2013
Publication Date
May 1, 1969
Subject Category
Propellants
Report/Patent Number
NASA-CR-101935
Report Number: NASA-CR-101935
Accession Number
69N38790
Funding Number(s)
CONTRACT_GRANT: NAS9-6812
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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