NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Analyses for the description of rocket and airbreathing propulsion system combustion chamber and nozzle flows Annual reportCalculations of rocket and air breathing propulsion system combustion chamber and nozzle flow performance
Document ID
19700027042
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Edelman, R. B.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Fortune, O. F.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Weilerstein, G.
(General Applied Science Labs., Inc. Westbury, NY, United States)
Date Acquired
August 5, 2013
Publication Date
April 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
GASL-TR-736
NASA-CR-102820
Report Number: GASL-TR-736
Report Number: NASA-CR-102820
Accession Number
70N36358
Funding Number(s)
CONTRACT_GRANT: NAS8-21387
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available