This task is to hot-fire test an existing Space Launch Mission (SLM) injector that is applicable for all expander cycle engines being considered for the exploration upper stage. The work leverages investment made in FY 2013 that was used to additively manufacture three injectors (fig. 1) all by different vendors..


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    Title :

    Hot-Fire Test of Liquid Oxygen/Hydrogen Space Launch Mission Injector Applicable to Exploration Upper Stage


    Contributors:


    Publication date :

    2015-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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    Creech S. D. / Crumbly C. M. / Robinson K. F. | NTIS | 2015


    NASA's Space Launch System Mission Capabilities for Exploration

    Creech, Stephen D. / Crumbly, Christopher M. / Robinson, Kimberly F. | NTRS | 2015


    NASA'S Space Launch System Mission Capabilities for Exploration

    Creech S. D. / Crumbly C. M. / Robinson K. F. | NTIS | 2015


    NASA'S Space Launch System Mission Capabilities for Exploration

    Creech, Stephen D. / Crumbly, Christopher M. / Robinson, Kimberly F. | NTRS | 2015