Effect of temperature and O-ring gland finish on sealing ability of Viton V747-75

As a part of the redesign project of the Space Shuttle solid rocket motor (SRM) following the Challenger accident, the field joint was redesigned to minimize the relative joint motion caused by internal motor pressurization during ignition. The O-ring seals and glands for the field joint were design...

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Bibliographische Detailangaben
1. Verfasser: Lach, Cynthia L.
Format: Report
Sprache:eng
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