• 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