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
Link To Document :
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