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Centaur operations at the space stationA study was conducted on the feasibility of using a Centaur vehicle as a testbed to demonstrate critical OTV technologies at the Space Station. Two Technology Demonstration Missions (TDMs) were identified: (1) Accommodations, and (2) Operations. The Accommodations TDM contained: (1) berthing, (2) checkout, maintenance and safing, and (3) payload integration missions. The Operations TDM contained: (1) a cryogenic propellant resupply mission, and (2) Centaur deployment activities. A modified Space Station Co-Orbiting Platform (COP) was selected as the optimum refueling and launch node due to safety and operational considerations. After completion of the TDMs, the fueled Centaur would carry out a mission to actually test deployment and help offset TDM costs. From the Station, the Centaur could carry a single payload in excess of 20,000 pounds to geosynchronous orbit or multiple payloads.
Document ID
19880016089
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Porter, J.
(General Dynamics/Astronautics San Diego, CA, United States)
Thompson, W.
(General Dynamics/Astronautics San Diego, CA, United States)
Bennett, F.
(General Dynamics/Astronautics San Diego, CA, United States)
Holdridge, J.
(General Dynamics/Astronautics San Diego, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 15, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-179593
NAS 1.26:179593
GDSS-SP-87-003
Report Number: NASA-CR-179593
Report Number: NAS 1.26:179593
Report Number: GDSS-SP-87-003
Accession Number
88N25473
Funding Number(s)
PROJECT: RTOP 480-52-02
CONTRACT_GRANT: NAS3-24900
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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