11 research outputs found

    Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1

    Get PDF
    Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limit

    Effect of water vapor on H sub 2-O sub 2 detonations.

    No full text

    The influence of water vapor addition on hydrogen-oxygen detonations

    Full text link
    http://deepblue.lib.umich.edu/bitstream/2027.42/5981/5/bac5840.0001.001.pdfhttp://deepblue.lib.umich.edu/bitstream/2027.42/5981/4/bac5840.0001.001.tx
    corecore