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Quick look test report: MPT static firing no. 2 test MPT-S2The three engine cluster was fired at 70 percent power level for a nominal 15 seconds to evaluate the integrated performance of the main propulsion system. Engine ignition occurred at approximately 1403 with the planned mainstage duration achieved for all three engines. Operation of all systems was as expected with the exception of the recirculation pumps. The pumps were started while the propellant loading was in fast fill, but they cavitated and lost head at the termination of fast fill. The pumps were subsequently restarted after pressurizing the tank and draining back propellant to get good quality. Post test inspection of the engines revealed some discoloration on the inside of the thrust chamber and distorted drain lines for engine #2.
Document ID
19780021198
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
June 12, 1978
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-151814
SD-78-SH-0125
Report Number: NASA-CR-151814
Report Number: SD-78-SH-0125
Accession Number
78N29141
Funding Number(s)
CONTRACT_GRANT: NAS9-14000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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