FIELD: rocketry.
SUBSTANCE: proposed solid-propellant rocket engine contains housing with channel charge, charge fitted in channel and igniter including housing with one of several nozzles-holes. Exit section of nozzle-hole of igniter is located at distance equal to 2-8 equivalent diameters of nozzle-hole from ignited surface of charge. Angle of tilting of axis of nozzle-hole to ignited surface is not less than 45°.
EFFECT: reduced mass of igniting composition required for operation of engine.
2 dwg
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2008 |
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