• DocumentCode
    3200472
  • Title

    Planetary sample sealing for caching

  • Author

    Backes, Paul ; Onstott, Tullis ; Bar-Cohen, Yoseph ; Badescu, Mircea ; Pratt, Lisa ; Helmick, Daniel ; Sherrit, Stewart ; Johnson, Adam ; Bao, Xiaoqi

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    10
  • Abstract
    A sample sealing technique was developed and tested for a possible Mars Sample Return mission application. The effect on the scientific viability of biological samples from storage of samples in a sample container for a long period of time on the Martian surface was also investigated. Sealing techniques were investigated and a soldering concept was developed and tested to provide a hermetic seal between a sample tube and cap. A sample caching subsystem design concept was updated to allow for sealing of sample tubes. A gas-tight vessel was constructed that could be used to simulate environmental conditions that would be experienced by a sample of regolith on Mars and to test the affects of thermal cycling of the vessel on psychrophilic microorganisms embedded in a regolith simulant to assess the degree of deterioration of the microorganisms.
  • Keywords
    Mars; aerospace biophysics; microorganisms; planetary rovers; planetary surfaces; seals (stoppers); soldering; space research; specimen preparation; storage; Mars sample return mission; Martian surface; biological samples scientific liability; caching; gas-tight vessel; microorganism deterioration degree; planetary sample sealing; psychrophilic microorganisms; sealing technique; soldering; thermal cycling; Coils; Containers; Fabrication; Geology; Hermetic seals; Mars; Microorganisms; Sealing materials; Soldering; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839307
  • Filename
    4839307