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Localized overheating in Aerobee regeneratively cooled thrust chambersOverheating in convergent section of Aerobee rocket combustion chamber nozzle due to nozzle design and regenerative cooling system
Document ID
19660021049
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bushnell, P. S., Jr. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Busse, J. R. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
X-721-66-146
NASA-TM-X-55516
Report Number: X-721-66-146
Report Number: NASA-TM-X-55516
Accession Number
66N30339
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE
AEROBEE ROCKET
CONVERGENT NOZZLE
ROCKET ENGINE
COMBUSTION CHAMBER
REGENERATIVE COOLING

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