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Storable orbit transfer vehicleOrbit transfer vehicles (OTV) are evaluated against mission model requirement. Mission suitability of OTVs using storable propellant, cryogenic propellant, and electric propulsion systems is outlined. Energy required, g-level, spacecraft deploy/return, operational constraints, mission duration, and packaging are considered.
Document ID
19820019489
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pipes, W. E. (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
82N27365
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820019482Collected WorksLarge Space Systems/Propulsion Interactions
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