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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    Title :

    Apollo 12 mission report. Supplement 4: Ascent propulsion system final flight evaluation


    Contributors:

    Publication date :

    1972-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :