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The use of low power dual mode nuclear thermal rocket engines to support space exploration missionsThe evolution of dual mode concepts is presented, focusing on advantages and problems associated with both low and high temperature dual mode conversion systems. It is concluded that dual mode nuclear thermal rocket (NTR) systems using high temperature Brayton cycle conversion technology offer a high payoff enhancement of conventional NTR, with a comparatively minor increase of technological challenge. It is recommended that NTR engines be designed so that dual mode conversion systems can be attached to them in a modular way, thus enabling the production of electric power on all missions where it is needed.
Document ID
19910067707
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zubrin, Robert M.
(Martin Marietta Astronautics Group Denver, CO, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 91-3406
Accession Number
91A52330
Distribution Limits
Public
Copyright
Other

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