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Title: PERFORMANCE OF TWO LIQUID METAL TURBOPROP ENGINES UTILIZING A CIRCULATING FUEL REACTOR

Technical Report ·
OSTI ID:4792061

The performance of two all-nuclear turboprop engines utilizing the circulating fuel reactor with a fluoride fuel temperature of I500 deg F was investigated. Data are presented for off-match-point and modified match-point performances. Results are given in graph form. (M.C.G.)

Research Organization:
Pratt and Whitney Aircraft Div., United Aircraft Corp., Hartford, Conn.
DOE Contract Number:
AT(11-1)-229
NSA Number:
NSA-16-015917
OSTI ID:
4792061
Report Number(s):
PWAC-118
Resource Relation:
Other Information: Orig. Receipt Date: 31-DEC-62
Country of Publication:
United States
Language:
English