FIELD: rocket engines. SUBSTANCE: proposed method of assembly consists in placing insert charge in engine body. Loading the charge is effected in thin-walled smooth sleeve which is withdrawn after loading. Charge is unrestricted over lateral surface. EFFECT: enhanced safety and improved quality of assembly of solid- propellant rocket engines. 2 dwg
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Authors
Dates
2002-06-20—Published
2001-02-05—Filed