Cryopump for Large Pulses of Hydrogen

B C Moore; R G Camarillo; J. T. Morrow

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NASA NTRS · 19820017421

Cryopump for Large Pulses of Hydrogen

B C Moore·R G Camarillo·J. T. Morrow

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Abstract

A test involving a flow of hot hydrazine decomposition products at a rate of 13.6 g/s (0.03 lb/s) established the requirement to maintain pressure in an 11.9-m-(39 ft) diameter space chamber below 200 microns. The flow, 2/3 hydrogen and 1/3 nitrogen by volume, continued for several periods ranging from 3 to 15 min. The pressure requirement was necessary to minimize thermal effects of the gas on the test vehicle but was well beyond the capability of the existing facility pumps. Various methods of obtaining additional temporary jump capacity were considered. From these, the slugged-charcoal approach was selected as the quickest and least expensive method to implement.

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B C Moore, R G Camarillo, J. T. Morrow. 1982-01-01. Cryopump for Large Pulses of Hydrogen. https://ntrs.nasa.gov/citations/19820017421

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