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NASA NTRS · 19960022547

Space Shuttle Main Engine Propellant Path Leak Detection Using Sequential Image Processing

L Montgomery Smith·Jo Anne Malone·Roger A Crawford
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Abstract

Initial research in this study using theoretical radiation transport models established that the occurrence of a leak is accompanies by a sudden but sustained change in intensity in a given region of an image. In this phase, temporal processing of video images on a frame-by-frame basis was used to detect leaks within a given field of view. The leak detection algorithm developed in this study consists of a digital highpass filter cascaded with a moving average filter. The absolute value of the resulting discrete sequence is then taken and compared to a threshold value to produce the binary leak/no leak decision at each point in the image. Alternatively, averaging over the full frame of the output image produces a single time-varying mean value estimate that is indicative of the intensity and extent of a leak. Laboratory experiments were conducted in which artificially created leaks on a simulated SSME background were produced and recorded from a visible wavelength video camera. This data was processed frame-by-frame over the time interval of interest using an image processor implementation of the leak detection algorithm. In addition, a 20 second video sequence of an actual SSME failure was analyzed using this technique. The resulting output image sequences and plots of the full frame mean value versus time verify the effectiveness of the system.

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BibTeXRIS

L Montgomery Smith, Jo Anne Malone, Roger A Crawford. 1995-01-15. Space Shuttle Main Engine Propellant Path Leak Detection Using Sequential Image Processing. https://ntrs.nasa.gov/citations/19960022547

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