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Manned geosynchronous mission requirements and systems analysis study. Volume 1: Executive summaryThe crew capsule of the MOTV was studied with emphasis on crew accommodations, crew capsule functional requirements, subsystem interface definition between crew module and propulsion module, and man rating requirements. Competing mission modes were studied covering a wide range of propulsion concepts. These included one stage, one and one half stage, and two stage concepts using either the standard STS or an augmented STS. Several deorbit concepts were considered, including all propulsive modes, direct re-entry, and aeromaneuvering skip in skip out in the upper reaches of Earth's atmosphere. A five year plan covering costs, schedules, and critical technology issues is discussed.
Document ID
19800006927
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Boyland, R. E.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Sherman, S. W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Morfin, H. W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 4, 2013
Publication Date
November 7, 1979
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-160429
Accession Number
80N15186
Funding Number(s)
CONTRACT_GRANT: NAS9-15779
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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