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. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Skylab Program Csm Verification Analysis Report


    Contributors:

    Publication date :

    1970


    Size :

    88 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Skylab program CSM verification analysis report

    Schaefer, J. L. / Vanderpol, G. A. | NTRS | 1970





    Skylab Film Usage Analysis Program

    R. A. Schlagheck | NTIS | 1971