DocumentCode
790027
Title
Instrumentation for Nuclear Rocket Engines
Author
Gilles, W.P.
Author_Institution
Aerojet-General Corporation Sacramento, California
Volume
16
Issue
1
fYear
1969
Firstpage
266
Lastpage
270
Abstract
The NERVA program presents many difficult instrumentation design problems. Gamma fluxes reach 109 rads(C)/hr and neutron fluences approach 1018 n/cm2 (E>l.0 Mev), while temperatures range from 40 to 4500°R. A summary of these problems and their solutions is discussed.
Keywords
Cables; Engines; Gamma rays; Hydrogen; Inductors; Instruments; Neutrons; Propulsion; Rockets; Temperature measurement;
fLanguage
English
Journal_Title
Nuclear Science, IEEE Transactions on
Publisher
ieee
ISSN
0018-9499
Type
jour
DOI
10.1109/TNS.1969.4325117
Filename
4325117
Link To Document