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System Requirements and Operations Panel Workshop summaryThe low Earth orbit (LEO) versus the geosynchronous Earth orbit (GEO) deployment systems were discussed. The following items are emphasized: (1) large area systems, such as deployment, altitude, orbit transfer, and on orbit operation; (2) propulsion oriented issues such as the orbit transfer vehicle and the auxiliary propulsion systems; (3) programmatic issues. The LEO versus GEO deployment is a significant driver on propulsion requirements for an orbit transfer vehicle. It is suggested that early systems will be deployed at LEO. The Shuttle remote manipulator system (RMS) will not be involved in early demonstration activities. It is concluded that an integrated large space system/propulsion approach is essential and that propulsion development requirements need to be established.
Document ID
19820019497
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schwarzberg, F. R.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Large Space Systems(Propulsion Interactions
Subject Category
Spacecraft Propulsion And Power
Accession Number
82N27373
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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