Plasma ignition for laser propulsion
Abstract
For a specific optical system a pulsed carbon dioxide laser having an energy output of up to 15 joules was used to initiate a plasma in air at one atmosphere pressure. The spatial and temporal development of the plasma were measured using a multiframe image converter camera. In addition the time dependent velocity of the laser supported plasma front which moves opposite to the direction of the laser pulse was measured in order to characterize the type of wavefront developed. Reliable and reproducible spark initiation was achieved. The lifetime of the highly dense plasma at the initial focal spot was determined to be less than 100 nanoseconds. The plasma front propagates toward the laser at a variable speed ranging from zero to 1.6 x 1,000,000 m/sec. The plasma front propagates for a total distance of approximately five centimeters for the energy and laser pulse shape employed.
- Publication:
-
In NASA. Marshall Space Flight Center The 1982 NASA/ASEE Summer Fac. Fellowship Program 26 p (SEE N83-17359 07-80
- Pub Date:
- August 1982
- Bibcode:
- 1982asee.nasaR....A
- Keywords:
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- Cameras;
- Carbon Dioxide Lasers;
- Plasma Propulsion;
- Spark Ignition;
- Wave Fronts;
- Pulsed Lasers;
- Spacecraft Propulsion;
- Lasers and Masers