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Plasma ignition for laser propulsionFor 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.
Document ID
19830009093
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Askew, R. F.
(Auburn Univ. AL, United States)
Date Acquired
August 11, 2013
Publication Date
August 1, 1982
Publication Information
Publication: NASA. Marshall Space Flight Center The 1982 NASA(ASEE Summer Fac. Fellowship Program
Subject Category
Lasers And Masers
Accession Number
83N17364
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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