Search Results - Wadel, Mary F.

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  1. 1
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    Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber / by Wadel, Mary F.

    Published 1997
    Online Access
    Government Document eBook

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  2. 2
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    Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / by Wadel, Mary F.

    Published 1998
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    Government Document eBook

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  3. 3
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    Propulsion systems using in situ propellants for a Mars ascent vehicle by Wadel, Mary F.

    Published 1992
    Government Document Microfilm Book

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  4. 4
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    Validation of high aspect ratio cooling in a 89 kN (20,000 lb[sub f]) thrust combustion chamber by Wadel, Mary F.

    Published 1996
    Government Document Microfilm Book

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  5. 5
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    Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber / by Wadel, Mary F., Meyer, Michael L.

    Published 1996
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    Online Access
    Government Document eBook

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