NOZZLE STRUCTURE FOR COLD-WALL ROCKET NOZZLES Russian patent published in 2003 - IPC

Abstract RU 2213247 C2

FIELD: rocketry. SUBSTANCE: proposed structure consists of several elongated panels passing from inlet end to outlet end of nozzle and connected together along their longitudinal side edges. Large number of elongated parallel cooling channels is made in each wall, said channels being arranged longitudinally relative to panels. EFFECT: provision of light and strong reactive nozzle of simple design and easy to manufacture. 8 cl, 6 dwg

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RU 2 213 247 C2

Authors

Kheggander Jan

Dates

2003-09-27—Published

1998-11-27—Filed