Vacuum Leakage Tests of a Simulated Lightweight Spacecraft Air Lock

Vacuum Leakage Tests of a Simulated Lightweight Spacecraft Air Lock PDF

Author: Otto F. Trout (Jr.)

Publisher:

Published: 1970

Total Pages: 50

ISBN-13:

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A lightweight simulated spacecraft air-lock structure was tested under high vacuum to evaluate structural sealing problems and to determine leakage rates. Three different types of hatch configurations and three different seal configurations were tested for a temperature range of from -40° F (-40° C) to 200' F (930 C). Leakage rates of less than 1 x cc/sec or less than 10 (to the power of negative 4) cc/day of helium (standard temperature and pressure) were attained for each hatch.

Monthly Catalog, United States Public Documents

Monthly Catalog, United States Public Documents PDF

Author: United States. Superintendent of Documents

Publisher:

Published: 1968

Total Pages: 1716

ISBN-13:

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February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index