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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    Titel :

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


    Beteiligte:
    Smith, R. J. (Autor:in) / Wood, S. C. (Autor:in)

    Erscheinungsdatum :

    1972-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :