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
Analytical and experimental study of altitude compensation of a rocket by secondary injectionAltitude compensation and thrust augmentation studied in mixing effects of supersonic flows of rocket engine
Document ID
19660024206
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-66155
Report Number: NASA-CR-66155
Accession Number
66N33496
Funding Number(s)
CONTRACT_GRANT: NAS1-4102
CONTRACT_GRANT: NAS1-2962
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUST AUGMENTATION
MIXED FLOW
ALTITUDE CONTROL
SUPERSONIC FLOW
ROCKET ENGINE

Related Records

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