DocumentCode
2578734
Title
Digital MicroPropulsion
Author
Lewis, D.H., Jr. ; Janson, S.W. ; Cohen, R.B. ; Antonsson, E.K.
Author_Institution
TRW Inc., Redondo Beach, CA, USA
fYear
1999
fDate
21-21 Jan. 1999
Firstpage
517
Lastpage
522
Abstract
Arrays of "Digital Propulsion" micro-thrusters have been fabricated and tested. A three-layer sandwich is fabricated containing micro-resistors, thrust chambers, and rupture diaphragms. A propellant is loaded into the chambers, which are then sealed. When the resistor is heated sufficiently, the propellant ignites raising the pressure in the chamber and rupturing the diaphragm. An impulse is imparted as the high-pressure fluid is expelled from the chamber. On the order of 10/sup 6/ thrusters can be fabricated on a single wafer. Initial tests, using lead styphnate as the propellant, have produced 10/sup -4/ Newton-seconds of impulse and about 100 Watts of power.
Keywords
aerospace propulsion; diaphragms; micromechanical devices; 100 W; Digital MicroPropulsion; MEMS space system; lead styphnate propellant; microresistor; microthruster array; rupture diaphragm; Aerospace testing; Bonding; Fuels; Glass; Micromechanical devices; Propulsion; Rockets; Space technology; Space vehicles; Valves;
fLanguage
English
Publisher
ieee
Conference_Titel
Micro Electro Mechanical Systems, 1999. MEMS '99. Twelfth IEEE International Conference on
Conference_Location
Orlando, FL, USA
ISSN
1084-6999
Print_ISBN
0-7803-5194-0
Type
conf
DOI
10.1109/MEMSYS.1999.746882
Filename
746882
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