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The NASA low thrust propulsion programThe NASA OAST Propulsion, Power, and Energy Division supports a low thrust propulsion program aimed at providing high performance options for a broad range of near-term and far-term mission and vehicles. Low thrust propulsion has a major impact on the mission performance of essentially all spacecraft and vehicles. On-orbit lifetimes, payloads, and trip times are significantly impacted by low thrust propulsion performance and integration features for Earth-to-orbit (ETO) vehicles, Earth-orbit and planetary spacecraft, and large platforms in Earth orbit. Major emphases are on low thrust chemical propulsion, both storables and hydrogen/oxygen; low-power (auxiliary) electric arcjects and resistojets; and high-power (primary) electric propulsion, including ion, magnetoplasmadynamic (MPD), and electrodeless concepts. The major recent accomplishments of the program are presented and their impacts discussed.
Document ID
19890017524
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stone, James R.
(NASA Headquarters Washington, DC United States)
Bennett, Gary L.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 89-2492
E-4822
NAS 1.15:102065
NASA-TM-102065
Report Number: AIAA PAPER 89-2492
Report Number: E-4822
Report Number: NAS 1.15:102065
Report Number: NASA-TM-102065
Meeting Information
Meeting: Joint Propulsion Conference
Location: Monterey, CA
Country: United States
Start Date: July 10, 1989
End Date: July 12, 1989
Sponsors: ASEE, ASME, SAE, AIAA
Accession Number
89N26895
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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