NASA NTRS · 19730018123
Apollo 12 mission report. Supplement 4: Ascent propulsion system final flight evaluation
Abstract
The results of the postflight analysis of the ascent propulsion system (APS) performance during the Apollo 12 Mission are presented. The steady-state performance analysis, and pressurization system are discussed along with the propellant loading and usage, APS overburn, and burn time. It is concluded that APS flight performance reconstructions for LM-3, LM-4, LM-5, and LM-6 indicate that engine performance prediction techniques are conservative.
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Griffin, W. G.. 1972-09-01. Apollo 12 mission report. Supplement 4: Ascent propulsion system final flight evaluation. https://ntrs.nasa.gov/citations/19730018123
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