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US/CIS integrated NTREThe paper describes the Nuclear Thermal Energy (NTRE) engine, developed by taking advantage of mature fuel technology developed in the former Soviet Union, thus shortening the development schedule of this engine for moon and Mars explorations. The near-term NTRE engine has a number of features that provide safety, mission performance, cost, and risk benefits. These include: (1) high-temperature long-life CIS fuel, (2) high-pressure recuperated expander cycle, (3) assured restart, (4) long-life cooled nozzle with thin inner wall, (5) long-life turbopumps, (6) heat radiation and electrical power generation, and (7) component integration synergy. Diagrams of the reactor core, the recuperated bottoming cycle flow schematic, and the recuperated bottoming cycle engine schematic are presented.
Document ID
19930066141
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bulman, M. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Culver, D. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcilwain, M. C.
(Aerojet, Propulsion Div., Sacramento CA, United States)
Rochow, Richard
(Babcock & Wilcox Space and Nuclear Systems Lynchburg, VA, United States)
D'Yakov, E. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Smetannikov, V. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 93-2367
Report Number: AIAA PAPER 93-2367
Meeting Information
Meeting: AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: June 28, 1993
End Date: June 30, 1993
Sponsors: ASEE, ASME, AIAA, SAE
Accession Number
93A50138
Distribution Limits
Public
Copyright
Other

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