FIELD: machine building.
SUBSTANCE: invention relates to rocket propulsion units, namely, to solid-propellant rocket engines with charges from mixed solid fuels with inner combustion surface of star-like or similar shape, which are firmly fixed with heat-protective coating applied to the inner surface of the housing through protective-fixing layer. Solid-propellant rocket engine includes housing, heat-protective coating laid along its inner surface, end collars, protective-fixing layer and solid fuel charge. Along the entire length of the charge between the heat-insulating coating and the protective-fixing layer there is an intermediate layer of metal foil, which is evenly attached to the heat-insulating coating and the protective-fixing layer by an adhesive bond.
EFFECT: metal foil layer prevents penetration of gaseous components (ammonia) released into solid fuel charge from heat-insulating coating through protective-fixing layer during storage and operation, which prevents destruction of urethane and ester bonds of polydiene-urethane epoxy rubber, which is the base of charge of solid fuel, provides design traction characteristics during the whole operation of the solid-propellant rocket engine and improves reliability of engine operation.
1 cl, 2 dwg
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Authors
Dates
2020-01-23—Published
2018-12-19—Filed