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Nuclear Thermal Propulsion Requirements Analysis of the ESAS Reference Human Mars Mission ArchitectureThe Nuclear Thermal Propulsion Mission and System Analysis (NTP MSA) Phase 2 Study was initiated by Marshall Space Flight Center’s (MSFC) Advanced Concepts Office (VP11) in December, 2005 in support of MSFC’s Nuclear Systems Office (VP31) NTP for Exploration Study. The Mission and Systems Analysis Study was task # 6 of a set of 14 tasks within the NTP for Exploration Study. The primary goal of the NTP MSA
Phase 2 Study was to identify the range of potential NTP engine and vehicle requirements for NASA Exploration Systems Mission Directorate (ESMD) Mars human exploration reference mission.
Document ID
20240013888
Acquisition Source
Headquarters
Document Type
Other - Trade Study
Authors
Robert J. Hetterich
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
November 1, 2024
Publication Date
July 20, 2006
Subject Category
Aircraft Design, Testing and Performance
Funding Number(s)
CONTRACT_GRANT: NASA
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
mars
NTP
vehicle
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