• DocumentCode
    711230
  • Title

    Ensuring Cassini´s end-of-mission propellant margins

  • Author

    Sturm, Erick J. ; Barber, Todd J. ; Roth, Duane

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2015
  • fDate
    7-14 March 2015
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    The Cassini spacecraft is in its final years. On September 15, 2017, Cassini will plunge deep into Saturn´s atmosphere never to reemerge; thus concluding its second extended mission and 13 years in orbit around the ringed planet. As of October 2014, the spacecraft is four years in to its seven-year, second extended mission, the Cassini Solstice Mission (CSM). With three years left and only 2.5% of its loaded bipropellant and 37% of its loaded monopropellant remaining, the Cassini project actively manages the predicted end-of-mission propellant margins to maintain a high confidence in the spacecraft´s ability to complete the CSM as designed. Accurate spacecraft navigation, rigorous remaining-propellant estimation, and frequent future propellant consumption prediction have resulted in efficient propellant use and a probability of sufficient propellant margin greater than 99%.
  • Keywords
    Saturn; planetary atmospheres; probability; propellants; space vehicles; CSM; Cassini Solstice Mission; Cassini end-of-mission propellant margins; Cassini project; Cassini spacecraft; Saturn atmosphere; loaded monopropellant; probability; remaining-propellant estimation; second extended mission; spacecraft navigation; Fuels; Navigation; Orbits; Propulsion; Space vehicles; Trajectory; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2015 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4799-5379-0
  • Type

    conf

  • DOI
    10.1109/AERO.2015.7119015
  • Filename
    7119015