NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Dual-fuel, dual-throat engine preliminary analysisA propulsion system analysis of the dual fuel, dual throat engine for launch vehicle applications was conducted. Basic dual throat engine characterization data were obtained to allow vehicle optimization studies to be conducted. A preliminary baseline engine system was defined.
Document ID
19790023171
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, C. J. (Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-161304
REPT-32967F
Report Number: NASA-CR-161304
Report Number: REPT-32967F
Accession Number
79N31342
Funding Number(s)
CONTRACT_GRANT: NAS8-32967
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available