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Hybrid rocket propulsionTopics addressed are: (1) comparison of the theoretical impulses; (2) comparison of the density-specific impulses; (3) general propulsion system features comparison; (4) hybrid systems, booster applications; and (5) hybrid systems, upper stage propulsion applications.
Document ID
19930012913
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holzman, Allen L. (United Technologies Corp. San Jose, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Space Transportation Materials and Structures Technology Workshop. Volume 2: Proceedings
Subject Category
Spacecraft Propulsion And Power
Accession Number
93N22102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930012892Collected WorksSpace Transportation Materials and Structures Technology Workshop
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