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
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