DocumentCode
2068563
Title
Mission enabling and enhancing spacecraft capabilities with microNewton electric propulsion
Author
Marrese-Reading, Colleen M. ; Ziemer, John K. ; Scharf, Daniel P. ; Martin-Mur, Tomas J. ; Thompson, Paul ; Mueller, Juergen ; Wirz, Richard
Author_Institution
Jet Propulsion Lab., Pasadena, CA, USA
fYear
2010
fDate
6-13 March 2010
Firstpage
1
Lastpage
10
Abstract
The capability to significantly improve current spacecraft pointing, precision orbit maintenance and disturbance mitigation were considered using precision, quiescent microNewton electric propulsion systems. The results of the analyses showed that electric propulsion systems operating in the microNewton to hundreds of microNewtons thrust range can offer significant improvements over state-of-the-art mission capabilities to enable 30 m Earth-fixed orbital tubes, constellation spacecraft position control to within nanometers and exoplanet observatory pointing with 0.1 milliarcsecond precision. Electric propulsion thrust characteristics required to support these capabilities are discussed.
Keywords
Earth orbit; aircraft instrumentation; electric propulsion; position control; space vehicles; Earth-fixed orbital tubes; constellation spacecraft position control; current spacecraft pointing; disturbance mitigation; micro Newton electric propulsion system; precision orbit maintenance; Earth; Extrasolar planet; Extraterrestrial measurements; Frequency; Gravity; Observatories; Propulsion; Space missions; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2010 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-3887-7
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2010.5447032
Filename
5447032
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