Digital micropropulsion

Citation
Dh. Lewis et al., Digital micropropulsion, SENS ACTU-A, 80(2), 2000, pp. 143-154
Citations number
9
Categorie Soggetti
Instrumentation & Measurement
Journal title
SENSORS AND ACTUATORS A-PHYSICAL
ISSN journal
09244247 → ACNP
Volume
80
Issue
2
Year of publication
2000
Pages
143 - 154
Database
ISI
SICI code
0924-4247(20000310)80:2<143:DM>2.0.ZU;2-6
Abstract
Arrays of "Digital Propulsion" microthrusters have been fabricated and test ed. A three-layer sandwich is fabricated containing microresistors, thrust chambers, and rupture diaphragms. A propellant is loaded into each individu ally sealed chamber. When the resistor is energized, the propellant ignites , raising the pressure in the chamber and rupturing the diaphragm. An impul se is imparted as the high-pressure fluid is expelled from the chamber. On the order of 10(6) thrusters can be fabricated on a single wafer. Initial t ests, using lead styphnate as the propellant, have produced 10(-4) N s of i mpulse and about 100 W of power. (C) 2000 Elsevier Science S.A. All rights reserved.