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Small Satellite Propulsion OptionsAdvanced chemical and low power electric propulsion offer attractive options for small satellite propulsion. Applications include orbit raising, orbit maintenance, attitude control, repositioning, and deorbit of both Earth-space and planetary spacecraft. Potential propulsion technologies for these functions include high pressure Ir/Re bipropellant engines, very low power arcjets, Hall thrusters, and pulsed plasma thrusters, all of which have been shown to operate in manners consistent with currently planned small satellites. Mission analyses show that insertion of advanced propulsion technologies enables and/or greatly enhances many planned small satellite missions. Examples of commercial, DoD, and NASA missions are provided to illustrate the potential benefits of using advanced propulsion options on small satellites.
Document ID
19950005075
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, Roger M.
(NYMA, Inc. Brook Park, OH., United States)
Oleson, Steven R.
(NYMA, Inc. Brook Park, OH., United States)
Curran, Francis M.
(NASA Lewis Research Center Cleveland, OH, United States)
Schneider, Steven J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1994
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-9063
NASA-TM-106701
NAS 1.15:106701
AIAA PAPER 94-2997
Report Number: E-9063
Report Number: NASA-TM-106701
Report Number: NAS 1.15:106701
Report Number: AIAA PAPER 94-2997
Meeting Information
Meeting: Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: June 27, 1994
End Date: June 29, 1994
Accession Number
95N11488
Funding Number(s)
PROJECT: RTOP 506-32-03
CONTRACT_GRANT: NAS3-27186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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