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DOD low-thrust mission studiesThe space transportation system (STS) will be the principal means of launching USAF spacecraft beginning in the 1980's. Since it is manned and reusable it provides new opportunities for unique approaches for cost effective utilization of its capabilities. The STS also places additional requirements and constraints on advanced spacecraft deployment systems that did not previously exist for expandable launch vehicles. To fully utilize these new capabilities designers must be prepared by having cost effective technologies available. Advanced propulsion technology that would provide flexibility, performance, and economic benefits to future Air Force missions was identified. Both electric and chemical propulsion systems are discussed. An LO2/LH2 stage with a torus LO2 tank and 500 lbf pumb fed engine is high on the list of propulsion technology.
Document ID
19800022949
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pipes, W. E.
(Martin Marietta Corp. Bethesda, MD, United States)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Publication Information
Publication: NASA. Lewis Research Center Large Space Systems(Low-Thrust Propulsion Technol.
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N31455
Funding Number(s)
CONTRACT_GRANT: F04611-79-C-0032
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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