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Space station propulsion: The advanced development program at LewisA reference configuration was established for the initial operating capability (IOC) station. The reference configuration has assumed hydrazine fueled thrusters as the propulsion system. This was to establish costing and as a reference for comparison when other propulsion systems are considered. An integral part of the plan to develop the Space Station is the advanced development program. The objective of this program is to provide advanced technology alternatives for the initial and evolutionary Space Station which optimize the system's functional characteristics in terms of performance, cost, and utilization. The portion of the Advanced Development Program that is concerned with auxiliary propulsion and the research and programmatic activities conducted are discussed.
Document ID
19850017075
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:86999
E-2544
NASA-TM-86999
Report Number: NAS 1.15:86999
Report Number: E-2544
Report Number: NASA-TM-86999
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Monterey, CA
Country: United States
Start Date: July 8, 1985
End Date: July 10, 1985
Sponsors: SAE, AIAA, ASME
Accession Number
85N25386
Funding Number(s)
PROJECT: RTOP 482-50-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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