Multi-point ignition system for high-performance propulsion systems, in particular for ammunition
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United States of America Patent
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Apr 8, 2003
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N/A
app pub date -
Nov 20, 2000
filing date -
Nov 19, 1999
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Abstract
A high-performance propulsion system includes propellant charge powder arranged in a case (1) and multiple pyrotechnic igniters (9) for igniting the propellant charge powder, each igniter (9) containing a primer (5) and optionally a booster charge (6).
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