Phenomena, design concepts, and design problems related to emergency repressurization systems for 2 large-space simulation chambers designed to test Apollo vehicle and to train astronauts; repressurization systems protect astronauts from effects of sudden loss of space suit pressure and of breathing oxygen while chambers are under high vacuum; engineering problems encountered involving thermodynamics, transient heat transfer, high velocity gas flow, and acoustics; analyses and calculations indicate that present system design eliminated problems.
Emergency repressurization of large space simulation chambers
SAE -- Paper
SAE Meeting ; 1964 Simulators
1964
8 pages
Conference paper
English
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Emergency Repressurization of Large Space Simulation Chambers
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