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System requirementsRequirements of future space systems, including large space systems, that operate beyond the space shuttle are discussed. Typical functions required of propulsion systems in this operational regime include payload placement, retrieval, observation, servicing, space debris control and support to large space systems. These functional requirements are discussed in conjunction with two classes of propulsion systems: (1) primary or orbit transfer vehicle (OTV) and (2) secondary or systems that generally operate within or relatively near an operational base orbit. Three propulsion system types are described in relation to these requirements: cryogenic OTV, teleoperator maneuvering system and a solar electric OTV.
Document ID
19820019494
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Austin, R. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Lewis Research Center Large Space System(Propulsion Interactions
Subject Category
Spacecraft Propulsion And Power
Accession Number
82N27370
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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