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Teleoperator Maneuvering System (TMS) benefits assessment study. Volume 1: Executive summaryTeleoperator Maneuvering System (TMS) versus integral spacecraft propulsion, spacecraft maintenance, cost benefits, launch prices, integral propulsion length penalties, remote maintenance versus EVA, potential weight reduction benefits, basing mode, mission models and payload requirements, and program profitability are discussed.
Document ID
19830021763
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-170795
NAS 1.26:170795
Accession Number
83N30034
Funding Number(s)
CONTRACT_GRANT: NAS8-34888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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