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Ultimately Reliable Pyrotechnic SystemsThis paper presents the methods by which NASA has designed, built, tested, and certified pyrotechnic devices for high reliability operation in extreme environments and illustrates the potential applications in the oil and gas industry. NASA's extremely successful application of pyrotechnics is built upon documented procedures and test methods that have been maintained and developed since the Apollo Program. Standards are managed and rigorously enforced for performance margins, redundancy, lot sampling, and personnel safety. The pyrotechnics utilized in spacecraft include such devices as small initiators and detonators with the power of a shotgun shell, detonating cord systems for explosive energy transfer across many feet, precision linear shaped charges for breaking structural membranes, and booster charges to actuate valves and pistons. NASA's pyrotechnics program is one of the more successful in the history of Human Spaceflight. No pyrotechnic device developed in accordance with NASA's Human Spaceflight standards has ever failed in flight use. NASA's pyrotechnic initiators work reliably in temperatures as low as -420 F. Each of the 135 Space Shuttle flights fired 102 of these initiators, some setting off multiple pyrotechnic devices, with never a failure. The recent landing on Mars of the Opportunity rover fired 174 of NASA's pyrotechnic initiators to complete the famous '7 minutes of terror.' Even after traveling through extreme radiation and thermal environments on the way to Mars, every one of them worked. These initiators have fired on the surface of Titan. NASA's design controls, procedures, and processes produce the most reliable pyrotechnics in the world. Application of pyrotechnics designed and procured in this manner could enable the energy industry's emergency equipment, such as shutoff valves and deep-sea blowout preventers, to be left in place for years in extreme environments and still be relied upon to function when needed, thus greatly enhancing safety and operational availability.


Document ID
20150002925
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Scott, John H.
(NASA Johnson Space Center Houston, TX, United States)
Hinkel, Todd
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
March 13, 2015
Publication Date
May 4, 2015
Subject Category
Propellants And Fuels
Report/Patent Number
JSC-CN-32898
Report Number: JSC-CN-32898
Meeting Information
Meeting: Offshore Technology Conference (OTC )2015
Location: Houston, TX
Country: United States
Start Date: May 4, 2015
End Date: May 7, 2015
Sponsors: Baker Hughes Inteq
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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