REG NASA-LLIS-0966-1995 Lessons Learned Space Shuttle Main Engine (SSME) Fuel System Oscillations.pdf
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1、Lessons Learned Entry: 0966Lesson Info:a71 Lesson Number: 0966a71 Lesson Date: 1995-05-15a71 Submitting Organization: MSFCa71 Submitted by: Billy Cole / RetiredSubject: Space Shuttle Main Engine (SSME): Fuel System Oscillations Description of Driving Event: After the main fuel valve starts to open,
2、three oxidizer valves in the SSME are separately subjected to a series of position commands to precisely control oxidizer system priming times for the three combustors. The first oxidizer valve to be commanded is the fuel preburner oxidizer valve (FPOV). After a delay of 0.100 seconds, the FPOV is r
3、amped to 56 percent open at its maximum skew rate. At 0.72 seconds, the FPOV is given a “notch“ command to close about 10%. Just prior to the third fuel system oscillation, second “notch“ command is given.Lesson(s) Learned: Fuel system oscillations can be reduced during the startup phase by closely
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