FIELD: starting propulsion engine of projectiles and missiles after expelling from barrel or container. SUBSTANCE: engine has housing 1, insert charge 3 with open end surface 4 and igniter 5. Circular cavity 4 is formed between change 3 and inner surface 6 of housing. Nozzle support has through radial slots 8 on side of change. Circular chamber is gas-dynamically connected with igniter zone 9 through slots 8. EFFECT: enhanced reliability of rocket engine in course of ignition of change and attaining the mode. 2 dwg
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Authors
Dates
1998-05-20—Published
1995-03-28—Filed