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Feasibility of obtaining hypervelocity acceleration using propellant lined launch tubes Final report, 27 Sep. 1966 - 5 May 1970Feasibility of explosive lining in launch tube for hypervelocity projectile acceleration
Document ID
19710004558
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rodenberger, C. (Texas A&M Univ. College Station, TX, United States)
Sawyer, M. L. (Texas A&M Univ. College Station, TX, United States)
Tower, M. M. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-108699
Report Number: NASA-CR-108699
Accession Number
71N14033
Funding Number(s)
CONTRACT_GRANT: NAS9-6812
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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