The command and service module 112 service propulsion system performance for the Apollo 15 mission was evaluated and found to be satisfactory. The following items were considered: (1) the steady-state performance as determined from analysis of the third and eight burns; (2) techniques, problems, and assumptions; (3) flight analysis results as compared to the preflight predicted performance; (4) the propellant utilization and gaging system operation; (5) the pressurization system performance; (6) transient data; and (7) revision of estimated propellant consumption.


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    Title :

    Apollo 15 mission report. Supplement 2: Service propulsion system final flight evaluation


    Contributors:
    Smith, R. J. (author) / Wood, S. C. (author)

    Publication date :

    1972-11-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :