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Non-Intrusive Sensor for In-Situ Measurement of Recession Rate of Ablative and Eroding MaterialsA non-intrusive sensor for in-situ measurement of recession rate of heat shield ablatives. An ultrasonic wave source is carried in the housing. A microphone is also carried in the housing, for collecting the reflected ultrasonic waves from an interface surface of the ablative material. A time phasing control circuit is also included for time-phasing the ultrasonic wave source so that the waves reflected from the interface surface of the ablative material focus on the microphone, to maximize the acoustic pressure detected by the microphone and to mitigate acoustic velocity variation effects through the material through a de-coupling process that involves a software algorithm. A software circuit for computing the location off of which the ultrasonic waves scattered to focus back at the microphone is also included, so that the recession rate of the heat shield ablative may be monitored in real-time through the scan-focus approach.
Document ID
20150003182
Acquisition Source
Ames Research Center
Document Type
Other - Patent
Authors
Papadopoulos, George
Tiliakos, Nicholas
Benel, Gabriel
Thomson, Clint
Date Acquired
March 18, 2015
Publication Date
January 14, 2014
Subject Category
Computer Programming And Software
Instrumentation And Photography
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-8,627,724
Patent Application Number: US-Patent-Appl-SN-13/224,214
Funding Number(s)
CONTRACT_GRANT: NNA08BA27C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,627,724
Patent Application
US-Patent-Appl-SN-13/224,214
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