• DocumentCode
    2063764
  • Title

    Cassini Main Engine Assembly cover flight management and performance

  • Author

    Somawardhana, Ruwan P. ; Millard, Jerry M.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    20
  • Abstract
    The Cassini spacecraft has performed its four year Prime Mission at Saturn and is currently in orbit at Saturn performing a two year extended mission. Its main engine nozzles are susceptible to impact damage from micrometeoroids and on-orbit dust. The spacecraft has an articulating device known as the Main Engine Assembly (MEA) cover which can close and shield the main engines from these threats. The cover opens to allow for main engine burns that are necessary to maintain the trajectory. Periodically updated analyses of potential on-orbit dust hazard threats have resulted in the need to continue to use the MEA cover beyond its intended use and beyond its design life. This paper provides a detailed Systems-level overview of the flight management of the MEA cover device and its flight performance to date.
  • Keywords
    Saturn; aerospace engines; nozzles; space vehicles; Cassini spacecraft; Saturn; engine nozzles; impact damage; main engine assembly cover flight management; micrometeoroids; on-orbit dust hazard threats; Assembly; Coatings; Engines; Hardware; Instruments; Laboratories; Moon; Propulsion; Saturn; 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.2010.5446846
  • Filename
    5446846