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PIEZO-RESONANCE IGNITER AND IGNITION METHOD FOR PROPELLANT LIQUID ROCKET ENGINE

  • US 20090173321A1
  • Filed: 01/17/2006
  • Published: 07/09/2009
  • Est. Priority Date: 01/17/2006
  • Status: Active Grant
First Claim
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1. An ignition system for a combustor comprising:

  • a resonance system;

    a piezoelectric system driven by said resonance system; and

    an igniter powered by said piezoelectric system.

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