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Gamma heating in reflector heat shield of gas core reactorHeating rate measurements made in a mock-up of a BeO heat shield for a gas core nuclear rocket engine yields results nominally a factor of two greater than calculated by two different methods. The disparity is thought to be caused by errors in neutron capture cross sections and gamma spectra from the low cross-section elements, D, O, and Be.
Document ID
19720026001
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lofthouse, J. H.
(Aerojet Nuclear Co. Idaho Falls, ID, United States)
Kunze, J. F.
(Aerojet Nuclear Co. Idaho Falls, ID, United States)
Young, T. E.
(Aerojet Nuclear Co. Idaho Falls, ID, United States)
Young, R. C.
(Aerojet Nuclear Co. Idaho Falls, ID, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-CR-120903
ANCR-1077
Report Number: NASA-CR-120903
Report Number: ANCR-1077
Accession Number
72N33651
Funding Number(s)
CONTRACT_GRANT: NASA ORDER C-54558-B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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