• DocumentCode
    324968
  • Title

    Micromechanical devices at JPL for space exploration

  • Author

    Tang, William C.

  • Author_Institution
    Center for Space Microelectron. Technol., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    1
  • fYear
    1998
  • fDate
    21-28 Mar 1998
  • Firstpage
    461
  • Abstract
    Space exploration in the coming century will emphasize cost effectiveness and highly focused mission objectives, which will result in frequent multiple missions that broaden the scope of space science and to validate new technologies on a timely basis. Micro electromechanical systems (MEMS) is one of the key enabling technologies to create cost-effective, ultra-miniaturized, robust, and functionally focused spacecraft for both robotic and human exploration programs. Examples of MEMS devices at various stages of development include microgyroscope, microseismometer, microhygrometer, quadrupole mass spectrometer, and micropropulsion engine. These devices, when proven successful, will serve as models for developing components and systems for new-millennium spacecraft
  • Keywords
    aerospace propulsion; gyroscopes; mass spectrometers; micromechanical devices; seismometers; space vehicle electronics; JPL; MEMS; enabling technologies; functionally focused spacecraft; microgyroscope; micromechanical devices; micropropulsion engine; microseismometer; quadrupole mass spectrometer; space exploration; Costs; Electromechanical systems; Humans; Micromechanical devices; Orbital robotics; Robustness; Space exploration; Space missions; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 1998 IEEE
  • Conference_Location
    Snowmass at Aspen, CO
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-4311-5
  • Type

    conf

  • DOI
    10.1109/AERO.1998.686944
  • Filename
    686944