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Hybrid Propulsion Based on Fluid-Controlled Solid Gas GeneratorsThe use of fuel-rich solid (gas generator-type) propellants for hybrid propulsion affords some design and utilization efficiency advantages. Both forward and aft liquid injection control concepts are evaluated form the operational standpoints of ballistics, throttling, Stability and extinguishment.
Document ID
20210004512
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/35344
Authors
Strand, Leon D.
Cohen, Norman S.
Date Acquired
June 28, 1993
Publication Date
June 28, 1993
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Propulsion
Hybrid

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