• 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