Sample return containerization and planetary protection using brazing for breaking the chain of contact to Mars

被引:0
|
作者
Bar-Cohen, Yoseph [1 ]
Badescu, Mircea [1 ]
Lee, Hyeong Jae [1 ]
Sherrit, Stewart [1 ]
Bao, Xiaoqi [1 ]
Shirajian, Nareg [1 ]
机构
[1] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
关键词
Sample return; planetary exploration; brazing; synchronous Sterilization; Separation; Seaming and Sealing (S4); break the chain (BTC); containerization; planetary protection;
D O I
10.1117/12.2581526
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Planetary protection of Mars samples returned to Earth in a future NASA mission is a critical part of preventing uncontrolled biological materials being released from the samples. The planetary protection process requires addressing the potential risks and would involve "breaking the chain of contact (BTC)", where any returned material reaching Earth for further analysis would have to be sealed inside a container with extremely high confidence. The sterilization process would require destroying any potential biological materials that may contaminate the external surface of the container. A novel process for containing the returned samples has been conceived and developed at JPL. The process consists of using induction heated brazing to synchronously sterilize, separate, seam and seal the container. In this case. the braze material is heated to the level of melting at temperatures higher than 500 degrees C in more than 0.5 sec to assure treating the exposed areas by meeting the NASA Procedural Requirements (NPR) document 8020.12D related to sterilization https://nodis3.gsfc.nasa.gov/npg img/N PR 8020 012D / N PR 8020 012D .pdf. The container that encloses the samples consists of double walls with interstitial space that is Earth-clean. The process consists of two-steps, where one was intended to be prepared on Earth and the second potentially executed on orbit around Mars. The latest results of this study that established the needed capability are described and discussed in this manuscript.
引用
收藏
页数:9
相关论文
共 48 条
  • [31] Planetary protection for a Europa surface sample return: The ice clipper mission
    McKay, CP
    [J]. SPACE LIFE SCIENCES: EXTRATERRESTRIAL ORGANIC CHEMISTRY, UV RADIATION ON BIOLOGICAL EVOLUTION, AND PLANETARY PROTECTION, 2002, 30 (06): : 1601 - 1605
  • [32] Sample Acquisition and Caching using Detachable Scoops for Mars Sample Return
    Younse, P.
    Stroupe, A.
    Huntsberger, T.
    Garrett, M.
    Eigenbrode, J. L.
    Benning, L. G.
    Fogel, M.
    Steele, A.
    [J]. 2009 IEEE AEROSPACE CONFERENCE, VOLS 1-7, 2009, : 103 - +
  • [33] Mars Sample Return Terminal Rendezvous State-Based Fault Protection
    Schulte, Peter Z.
    Spencer, David A.
    Goggin, McClain
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2020, 57 (01) : 187 - 197
  • [34] Planetary rover developments supporting Mars exploration, sample return and future human-robotic colonization
    Schenker, PS
    Huntsberger, TL
    Pirjanian, P
    Baumgartner, ET
    Tunstel, E
    [J]. AUTONOMOUS ROBOTS, 2003, 14 (2-3) : 103 - 126
  • [35] Planetary Rover Developments Supporting Mars Exploration, Sample Return and Future Human-Robotic Colonization
    Paul S. Schenker
    Terry L. Huntsberger
    Paolo Pirjanian
    Eric T. Baumgartner
    Eddie Tunstel
    [J]. Autonomous Robots, 2003, 14 : 103 - 126
  • [36] Mars Sample Return Using Commercial Capabilities: Mission Architecture Overview
    Gonzales, Andrew A.
    Stoker, Carol R.
    Lemke, Lawrence G.
    Bowles, Jeffrey V.
    Huynh, Loc C.
    Faber, Nicholas T.
    Race, Margaret S.
    [J]. 2014 IEEE AEROSPACE CONFERENCE, 2014,
  • [37] An efficient approach for Mars Sample Return using emerging commercial capabilities
    Gonzales, Andrew A.
    Stoker, Carol R.
    [J]. ACTA ASTRONAUTICA, 2016, 123 : 16 - 25
  • [38] Conceptual Design of Mars Sample Return Mission Using Solar Montgolfieres
    Biswal, Malaya Kumar M.
    Annavarapu, Ramesh Naidu
    [J]. 2021 IEEE AEROSPACE CONFERENCE (AEROCONF 2021), 2021,
  • [39] Mars Sample Return Using Commercial Capabilities: Propulsive Entry, Descent, and Landing
    Lemke, Lawrence G.
    Gonzales, Andrew A.
    Huynh, Loc C.
    [J]. 2014 IEEE AEROSPACE CONFERENCE, 2014,
  • [40] Finite element analysis of seal mechanism using SMA for Mars sample return
    Bao, Xiaoqi
    Younse, Paulo
    [J]. SENSORS AND SMART STRUCTURES TECHNOLOGIES FOR CIVIL, MECHANICAL, AND AEROSPACE SYSTEMS 2014, 2014, 9061