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Hot-Fire Test of Liquid Oxygen/Hydrogen Space Launch Mission Injector Applicable to Exploration Upper StageThis 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..
Document ID
20160008015
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Barnett, Greg (NASA Marshall Space Flight Center Huntsville, AL, United States)
Turpin, Jason (NASA Marshall Space Flight Center Huntsville, AL, United States)
Nettles, Mindy (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
June 29, 2016
Publication Date
January 1, 2015
Publication Information
Publication: George C. Marshall Space Flight Center Research and Technology Report 2014
Subject Category
Launch Vehicles And Launch Operations
General
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20150016165Collected WorksGeorge C. Marshall Space Flight Center Research and Technology Report 2014
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