• DocumentCode
    2787671
  • Title

    A review of the approach of NASA projects to planetary protection compliance

  • Author

    Barengoltz, Jack

  • Author_Institution
    Jet Propulsion Lab., Pasadena, CA, USA
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    253
  • Lastpage
    261
  • Abstract
    The approaches to planetary protection compliance by several space projects in the period between Galileo and the present are reviewed. The emphasis is on missions to Mars, based on the historical record and the specificity of planetary protection requirements for that planet. However, an interesting change in requirements dating back to Galileo´s launch led many years later to the protection of Europa and the choice of ending the mission with an entry into Jupiter. An analogy exists for Cassini at Saturn, with the potential for protecting Titan from the orbiter (not the Huygens probe of course). The Mars missions in the period include successes and failures. Planetary protection implementation is discussed for Mars observer, Mars pathfinder, Mars global surveyor, Mars polar lander, Mars climate orbiter, Mars odyssey, and Mars exploration rover. Next, some recent developments in planetary protection implementation for spacecraft being prepared for launch are presented. Finally, new planetary protection requirements adopted by COSPAR, which NASA is expected to follow, are described.
  • Keywords
    Mars; Saturn; astronomical techniques; space vehicles; Cassini; Europa protection; Galileo space projects; Huygens probe; Mars climate orbiter; Mars exploration rover; Mars global surveyor; Mars observer; Mars odyssey; Mars pathfinder; Mars polar lander; NASA projects; Saturn; Titan; planetary protection compliance; spacecrafts; Contamination; Earth; Laboratories; Mars; Moon; NASA; Propulsion; Protection; Space missions; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559319
  • Filename
    1559319