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oaioai:casi.ntrs.nasa.gov:19760008376

Oxygen boost pump study

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    Publication date
    1975
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    Abstract

    An oxygen boost pump is described which can be used to charge the high pressure oxygen tank in the extravehicular activity equipment from spacecraft supply. The only interface with the spacecraft is the +06 6.205 Pa supply line. The breadboard study results and oxygen tank survey are summarized and the results of the flight-type prototype design and analysis are presented

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    This paper was published in NASA Technical Reports Server.

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