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Multi-point ignition system for high-performance propulsion systems, in particular for ammunition










Image Number 2 for United States Patent #6543362.

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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