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A Low Cost Igniter Utilizing an SCB and Titanium Sub-Hydride Potassium Perchlorate PyrotechnicA conventional NSI (NASA Standard Initiator) normally employs a hot-wire ignition element to ignite ZPP (zirconium potassium perchlorate). With minor modifications to the interior of a header similar to an NSI device to accommodate an SCB (semiconductor bridge), a low cost initiator was obtained. In addition, the ZPP was replaced with THKP (titanium sub-hydride potassium perchlorate) to obtain increased overall gas production and reduced static-charge sensitivity. This paper reports on the all-fire and no-fire levels obtained and on a dual mix device that uses THKP as the igniter mix and a thermite as the output mix.
Document ID
19960020684
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
R. W. Bickes, Jr.
(Sandia National Laboratories Albuquerque, New Mexico, United States)
M. C. Grubelich
(Sandia National Laboratories Albuquerque, New Mexico, United States)
J. K. Hartman
(SCB Technologies Albuquerque, NM United States)
C. B. McCampbell
(SCB Technologies Albuquerque, NM United States)
J. K. Churchill
(Quantic-Holex Hollister, CA United States)
Date Acquired
August 17, 2013
Publication Date
February 8, 1994
Publication Information
Publication: Second NASA Aerospace Pyrotechnic Systems Workshop
Publisher: National Aeronautics and Space Administration
Issue Publication Date: January 1, 1984
Subject Category
Propellants And Fuels
Meeting Information
Meeting: 2nd NASA Aerospace Pyrotechnics Systems Workshop
Location: Albuquerque, NM
Country: US
Start Date: February 8, 1994
End Date: February 9, 1994
Sponsors: Stennis Space Center
Accession Number
96N24207
Funding Number(s)
CONTRACT_GRANT: DE-AC04-76DP-00789
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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