Thermal Analysis of Cryogenic Hydrogen Liquid Separator

During launch for the new Space Launch System (SLS) liquid hydrogen is bleed through the engines during replenish, pre-press, and extended pre-press to condition the engines prior to launch. The predicted bleed flow rates are larger than for the shuttle program. A consequence of the increased flow r...

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Bibliographische Detailangaben
Hauptverfasser: Congiardo, Jared F., Fortier, Craig R.
Format: Other
Sprache:eng
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