• DocumentCode
    2109285
  • Title

    Electronic packaging for extended Mars surface missions

  • Author

    Shapiro, Andrew A. ; Ling, Sharon X. ; Ganesan, Sanka ; Cozy, R. Scott ; Hunter, Donald J. ; Schatze, Donald V. ; Mojarradi, Mohammad M. ; Kolawa, Elizabeth A.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    4
  • fYear
    2004
  • fDate
    13-13 March 2004
  • Firstpage
    2515
  • Abstract
    Extended Mars missions require vehicles to survive a large number of extended temperature cycles. To address this issue for electronics, previous strategies have placed electronics in a "warm electronics box" where thermal management is more easily maintained. However, that strategy limits number and location of electronics. An alternative strategy allows electronics to be remotely located on actuator and wheel arms with no heating, which has the advantage of distributed control. This strategy requires the electronics to survive the Martian extremes of -120 to +20°C for the duration of the mission. In addition, wheel motor controllers were mounted directly on the motor casing extending the temperature range on the warm side to +85°C (including some margin). Since missions may last 18 months or more and with day-night cycles on Mars at about 26 hours this means exposure to approximately 500 cycles. Typical testing is performed to 3× the number of cycles giving the electronics a testing requirement of -120 to +85°C for 1,500 cycles. A chip on board strategy was selected and a parallel approach of materials characterization and physics of failure with engineering experimentation is being used to address the issues of a large temperature swing with many cycles. A full factorial experiment, designed to highlight expected failure modes from the physics of failure analysis, is being conducted. The experiment is designed to evaluate different substrate materials, different die attach materials and different encapsulants or coatings. Combinations of these materials are being evaluated on a test vehicle with a range of die sizes in an effort to determine lifetime and to verify failure modes. Initial results were presented.
  • Keywords
    Mars; actuators; aerospace control; aerospace testing; avionics; chip-on-board packaging; distributed control; failure analysis; machine control; planetary rovers; planetary surfaces; space vehicle electronics; thermal management (packaging); -120 to 85 degC; Mars surface missions; Martian extremes; actuator; aerospace testing; chip on board packaging; die attach materials; electronic packaging; encapsulant; engineering experimentation; failure analysis; failure mode verification; failure modes; large temperature swing; materials characterization; substrate materials; test vehicle; thermal management; warm electronics box; wheel arms; wheel motor controllers; Conducting materials; Electronic equipment testing; Electronic packaging thermal management; Electronics packaging; Mars; Physics; Temperature; Thermal management of electronics; Vehicles; Wheels;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2004. Proceedings. 2004 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-8155-6
  • Type

    conf

  • DOI
    10.1109/AERO.2004.1368046
  • Filename
    1368046