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Oxidizer heat exchangers for rocket engine operation in idle modesThe heat exchanger concept is discussed together with its role in rocket engine operation in idle modes. Two heat exchanger designs (low and high heat transfer) utilizing different approaches to achieve stable oxygen vaporization are presented as well as their performance test results. It is concluded that compact and lightweight heat exchangers can be used in a stable manner under the 'idle' operating conditions expected with the RL10 rocket engine.
Document ID
19870058144
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kanic, P. G.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Kmiec, T. D.
(Pratt and Whitney West Palm Beach, FL, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 87-2117
Accession Number
87A45418
Funding Number(s)
CONTRACT_GRANT: NAS3-24738
Distribution Limits
Public
Copyright
Other

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