NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
Combustion chamber PatentRegenerative cooling system for rocket combustion chamber using coolant tubes in convergent-divergent nozzle
Document ID
19710014492
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Gregory, J. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
August 12, 1969
Subject Category
Propulsion Systems
Report/Patent Number
Patent Number: NASA-CASE-XLE-04857
Patent Number: US-PATENT-3,460,759
Patent Application Number: US-PATENT-APPL-SN-621742
Accession Number
71N23968
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-XLE-04857|US-PATENT-3,460,759
Patent Application
US-PATENT-APPL-SN-621742

Related Records

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