FIELD: rocketry. SUBSTANCE: reduction of smoke upon completion of operation of solid-propellent engine is effected by cooling the inhibitory and thermal-protective coats by means of injection of liquid coolant which is subjected to heating before injection to temperature of its expansion, boiling and partial evaporation at pressure equal to 0.2-0.6 of mean pressure in combustion chamber. EFFECT: enhanced efficiency.
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Authors
Dates
1996-09-27—Published
1992-09-24—Filed