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Failure of Pyrotechnic Operated Valves with Dual InitiatorsInvestigation of recent pyrovalve failures reveals timing of redundant initiator firings is crucial for reliable operation of pyrovalves. Simultaneous firing, i.e., within a very narrow time frame, was found to be the primary cause of the valve failing to operate. Testing of both single and dual initiators revealed important design characteristics affecting pyrovalve device performance. They include Primer Chamber Assembly (PCA) geometry and material properties, as well as operational effects on combustion product flow, and resulting energy transfer to the booster. The CONAX PCA design has evolved slowly over time undergoing incremental changes to correct known issues. These piecewise changes were verified by limited test, without a full understanding of the overall system impact or effect on margins. Adequate system performance margins may be adversely affected in existing or future systems incorporating a pyrovalve actuated by simultaneous firing of dual initiators.
Document ID
20240000668
Acquisition Source
Langley Research Center
Document Type
Other - NESC Technical Bulletin No. 09-01 Approved by the NESC Review Board
Authors
Andreas Dibbern
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
January 16, 2024
Publication Date
September 1, 2009
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
Technical Bulletin No. 09-01
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Failure of Pyrotechnic Operated Valves
Dual Initiators
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