Even before the first flight of the Space Shuttle, it was understood low liquid hydrogen (LH2) Net Positive Suction Pressure (NPSP) at the inlet to the Space Shuttle Main Engine (SSME) can have adverse effects on engine operation. A number of failures within both the External Tank (ET) and the Orbiter Main Propulsion System could result in a low LH2 NPSP condition. Operational workarounds were developed to take advantage of the onboard crew s ability to manually throttle down the SSMEs, which alleviated the low LH2 NPSP condition. A throttling down of the SSME resulted in an increase in NPSP, mainly due to the reduction in frictional flow losses while at a lower throttle setting. As engineers refined their understanding of the NPSP requirements for the SSME (through a robust testing program), the operational techniques evolved to take advantage of these additional capabilities. Currently the procedure, which for early Space Shuttle missions required a Return-to-Launch-Site abort, now would result in a nominal Main Engine Cut Off (MECO) and no loss of mission objectives.
The Evolution of Utilizing Manual Throttles to Avoid Low LH2 NPSP at the SSME Inlet
AIAA SPACE 2011 Conference and Exposition ; 2011 ; Long Beach, CA, United States
01.01.2011
Aufsatz (Konferenz)
Keine Angabe
Englisch
The Evolution of Utilizing Manual Throttling to Avoid Excessively Low LH~2 NPSP at the SSME Inlet
British Library Conference Proceedings | 2011
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