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Annular nozzle engine technologyThe topics covered include: (1) driver rocket subsystem; (2) annular nozzle engine technology; (3) expansion-deflection nozzle; (4) aerospike-nozzled engine background; (5) aerospike testing; (6) linear aerospike; and (7) the combined cycle engine.
Document ID
19920012287
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Martinez, AL (Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA. Lewis Research Center, Rocket-Based Combined-Cycle (RBCC) Propulsion Technology Workshop. Tutorial Session
Subject Category
Spacecraft Propulsion And Power
Accession Number
92N21530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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