Altitude Testing of the J2-X engine at 100,000 feet (start capability). Chemical Steam Generation for providing vacuum. Project Started Mar 07. Test Stand Activation around Late 2010. J-2X Testing around early 2011.


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    Title :

    Altitude Testing of Large Liquid Propellant Engines


    Contributors:

    Conference:

    26th AIAA Aerodynamic Measurement Technology and Testing Conference Development of Test Facilities Session ; 2008 ; Seattle, WA, United States


    Publication date :

    2008-06-23


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Altitude Testing of Large Liquid Propellant Engines

    B. Maynard / N. Raines | NTIS | 2008


    Altitude Testing of Large Liquid Propellant Engines

    Maynard, Bryon / Raines, Nickey | AIAA | 2008


    Altitude Testing of Large Liquid Propellant Engines

    Maynard, Bryon T. / Raines, Nickey G. | NTRS | 2010


    Altitude Testing of Large Liquid Propellant Engines

    Maynard, B. / Raines, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008