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Molded composite pyrogen igniter for rocket motorsA lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain a pyrogen charge was designed for insertion into a rocket motor casing for ignition of the rocket motor charge. A molded plastic closure cap provided for the elongated tube includes an ignition charge for igniting the pyrogen charge and an electrically actuated ignition squib for igniting the ignition charge. The ignition charge is contained within a portion of the closure cap, and it is retained therein by a noncorrosive ignition pellet retainer or screen which is adapted to rest on a shoulder of the elongated tube when the closure cap and tube are assembled together. A circumferentially disposed metal ring is provided along the external circumference of the closure cap and is molded or captured within the plastic cap in the molding process to provide, along with O-ring seals, a leakproof rotary joint.
Document ID
19780016332
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Heier, W. C.
(NASA Langley Research Center Hampton, VA, United States)
Lucy, M. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 28, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LAR-12018-1
Patent Application Number: US-PATENT-APPL-SN-678520
Patent Number: US-PATENT-4,080,901
Accession Number
78N24275
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-12018-1|US-PATENT-4,080,901
Patent Application
US-PATENT-APPL-SN-678520
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