Deciprocforminicost_100107112756.pdf

spc_stnv_000227

"Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines."

Prior to acceptance of a liquid rocket engine for use in Saturn vehicles, the average thrust of two consecutive tests without an intervening calibration must satisfy specification requirements. The contractor may recalibrate after the first and subsequent tests if he so chooses, based upon decision limits, until the above requirement is met.

1965-10-01

Saturn V Collection

Box 15, Folder 9

University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama

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spc_stnv_000225_000249

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