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Development of propulsion for high atmospheric pressure or dense environmentsThe development of a propulsion system that employs a detonating propellant is described, and the need for such a system and its use in certain planetary atmospheres are demonstrated. A theoretical formulation of the relevant gas-dynamic processes was developed, and a related series of experimental tests were pursued.
Document ID
19730023132
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Varsi, G. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Back, L. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dowler, W. L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Publication Information
Publication: JPL Quart. Tech. Rev., Vol. 3, No. 2 (NASA-CR-133863)
Subject Category
Propulsion Systems
Accession Number
73N31864
Distribution Limits
Public
Copyright
Public Use Permitted.
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IDRelationTitle19730023126Collected WorksJPL Quarterly Technical Review, Volume 3, No. 2, July 1973
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