United States of America As Represented by the Secretary of the Air Force

Benjamin Sarka

Biswa N Ganguly

Siegfried H Hasinger

Peter Bletzinger

Larry P Goss

Alan Garscadden

Dennis F Grosjean

Robert A Olson

Sigmund W Kizirnis

A novel laser beam deflection system and method for temperature measurement of combustion flames of known composition is described which comprises a thin wire for placement at a predetermined location within the flame; a pulsed laser source for directing a pulsed beam onto the wire for heating the wire and immediately surrounding gases of the flame to produce an acoustic pulse in the flame; a pair of probe laser sources for directing parallel probe beams through the flame in predetermined spaced relationship to each other and to the wire, and a pair of detectors and associated electronics for detecting the respective deflections of the probe beams resulting from interactions with the pulse and measuring the time difference between respective deflections of the probe beams to determine the speed of the acoustic pulse through the flame and the temperature of the flame from the speed determination.

Non-perturbing beam deflection system and method for high repetition

A closed cycle, high repetition pulsed laser having a laser flow channel with an annular flow return surrounding the laser flow channel. Ultra high vacuum components and low out-gassing materials are used in the device. An externally driven axial flow fan is used for gas recirculation. A thyratron-switched low-inductance energy storage capacitor is used to provide a transverse discharge between profiled electrodes in the laser cavity.

Closed cycle annular-return gas flow electrical discharge laser

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Enon, OH, United States of America

Benjamin Sarka