• DocumentCode
    2789043
  • Title

    Planetary protection technology for Mars Sample Return

  • Author

    Gershman, Robert ; Adams, Marc ; Dillman, Robert ; Fragola, Joseph

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    996
  • Lastpage
    1005
  • Abstract
    The NASA Mars Exploration Program has recently adopted a plan that includes a first Mars Sample Return (MSR) mission proposed for launch in 2013. Such a mission would deal with two new categories of planetary protection requirements: (1) assuring a very low probability of inadvertent sample release in order to provide extra protection against the extremely unlikely possibility of biological hazards in the returned material; and (2) keeping the samples free of round-trip Earth organisms to facilitate evaluation after return to Earth. This paper describes the planetary-protection-related technical challenges awaiting any MSR mission and describes work in progress on technology needed to meet these challenges. New technology is needed for several functions. Containment assurance requires breaking the chain of contact with Mars: the exterior of the sample container must not be contaminated with Mars material either during the loading process or during launch from the Mars surface. Also, the sample container and its seals must survive the worst Earth impact corresponding to the candidate mission profile, the Earth return vehicle must provide accurate delivery to the Earth entry corridor, and the Earth entry vehicle must withstand the thermal and structural rigors of Earth atmosphere entry - all with an unprecedented degree of confidence. Sample contamination must be avoided by sterilizing the entire spacecraft, a challenge with modern avionics, or by sterilizing the sample collection and containment gear and then isolating it from other parts of the spacecraft.
  • Keywords
    Earth; Mars; aerospace safety; space research; space vehicles; Earth atmosphere entry; Earth entry corridor; Earth entry vehicle; Earth return vehicle; Mars Sample Return; Mars material; Mars surface; NASA Mars Exploration Program; biological hazards; containment assurance; containment gear; inadvertent sample release; modern avionics; planetary protection technology; returned material; round-trip Earth organisms; sample contamination; spacecraft sterilization; worst Earth impact; Biohazards; Biological materials; Containers; Earth; Hazardous materials; Mars; NASA; Protection; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559390
  • Filename
    1559390