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An accelerated development, reduced cost approach to lunar/Mars exploration using a modular NTR-based space transportation systemBenefits and rationale for developing a common, modular lunar/Mars space transporation system (STS) based on nuclear thermal rocket (NTR) are presented. The modular NTR is based on three key components including a 50 klbf NERVA-derived engine used in clusters of 2 or 3, two standardized tank sizes developed for the First Lunar Outpost and Mars cargo vehicle applications, and a preintegrated truss/propellant feed system used for transferring LH2 from the drop tanks into the 'in-line' tank. It is concluded that, by using these components in a 'building block' fashion, a variety of single and multi-engine lunar and Mars vehicles can be configured to satisfy particular mission requirements.
Document ID
19920074429
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Borowski, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Clark, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Sefcik, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Corban, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Alexander, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Astronautics (General)
Report/Patent Number
IAF PAPER 92-0574
Report Number: IAF PAPER 92-0574
Accession Number
92A57053
Distribution Limits
Public
Copyright
Other

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