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    COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM

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    COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM

    WASHINGTON, D.C., UNITED STATES

    08.27.2009

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    NASA

    COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM

    NASA Identifier: C-1955-38036

    IMAGE INFO

    Date Taken: 08.27.2009
    Date Posted: 02.08.2013 14:41
    Photo ID: 850927
    Resolution: 2100x2700
    Size: 2.07 MB
    Location: WASHINGTON, D.C., US
    Web Views: 3
    Downloads: 1

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