The application of the SINDA computer program for the transient thermodynamic simulation of the Apollo fuel cell/radiator system for the limit condition of the proposed Skylab mission is described. Results are included for the thermal constraints imposed upon the Pratt and Whitney fuel cell power capability by the Block 2 EPS radiator system operating under the Skylab fixed attitude orbits.


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    Titel :

    Skylab program CSM verification analysis report


    Beteiligte:

    Erscheinungsdatum :

    01.09.1970


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Skylab Program Csm Verification Analysis Report

    J. L. Schaefer / G. A. Vanderpol | NTIS | 1970





    Skylab Film Usage Analysis Program

    R. A. Schlagheck | NTIS | 1971