System (100) for supplying an igniter with propellant, comprising - a reservoir (10) having an intake (11) and a discharge (12), - a liquid propellant supply line connected to the intake (11) of the reservoir (10), - a propellant discharge line connecting a discharge (12) of the reservoir (10) to an igniter (40), characterized in that said reservoir (10) has an internal volume filled with heat storage spheres (20), said storage spheres (20) being designed to store heat and to transmit it to a fluid passing through said reservoir (10) so as to evaporate a liquid propellant passing through said reservoir (10).
SYSTEM FOR SUPPLYING AN IGNITER WITH PROPELLANT
2018-06-21
Patent
Electronic Resource
English
Igniter performance in solid-propellant rocket motors.
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