METHOD FOR MAKING OF SOLID-PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER HEAT INSULATION COAT Russian patent published in 2014 - IPC F02K9/34 

Abstract RU 2527224 C1

FIELD: machine building.

SUBSTANCE: heat protective coat is formed at mandrels to connect metal flange therewith for vulcanisation. Lengthwise and crosswise segments of 0.2-0.3 mm diameter nitinol wire pre-trained identically to flange curvature are uniformly applied on heat insulating material surface in flange zone after application of second and two last layers. Then other layers are applied to cure the thus formed stack.

EFFECT: higher reliability.

2 dwg

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RU 2 527 224 C1

Authors

Shajdurova Galina Ivanovna

Lobkovskij Sergej Anatol'Evich

Nesterov Boris Anatol'Evich

Oshchepkova Marina Jur'Evna

Kustov Mikhail Alekseevich

Dates

2014-08-27Published

2013-06-11Filed