Measuring and testing – Engine detonation – Combustion signal compared to reference signal varied by a...
Patent
1990-02-06
1993-12-28
Raevis, Robert
Measuring and testing
Engine detonation
Combustion signal compared to reference signal varied by a...
G01N 3322
Patent
active
052729087
ABSTRACT:
A sensitive instrument system for determining the position of the burn fr in a rocket motor is disclosed. Separate adjacent transmitter and receiver elements are attached to the rocket motor casing to form an ultrasonic interference system. An ultrasound beam is transmitted to the motor's interior and the reflected beam from the propellant gas burn front is captured by the receiver. The received signal is processed to determine the distance to the propellant-gas interface.
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Raevis Robert
The United States of America as represented by the Secretary of
Warsh Kenneth L.
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