Development of an advanced failure detection algorithm for the SSMESince ground testing of the Space Shuttle Main Engine began in 1975, a multifaceted detection/shutdown system has been used to detect engine anomalies and initiate shutdown. In spite of this system, 27 major incidents have occurred since testing began. Although a small percentage of over 1200 successful hot fire tests, such incidents can result in significant cost and schedule impacts. Therefore, an advanced failure detection algorithm has been developed which consists of three detection approaches designed for a failure characteristic that has been previously documented. Simulations using sensor data from five incident tests show the algorithm detecting an anomally and signalling shutdown prior to the redline cutoff time. The foundation elements of the algorithm and its functioning are described.
Document ID
19880060823
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Norman, A. (Rockwell International Corp. Canoga Park, CA, United States)
Taniguchi, M. (Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 88-3408Report Number: AIAA PAPER 88-3408