ROCKET SOLID FUEL CHARGE Russian patent published in 2010 - IPC F02K9/18 

Abstract RU 2391530 C1

FIELD: machine building.

SUBSTANCE: rocket solid fuel charge consists of case, of protective-fixing layer, of end collars, of head half-charge with star-shaped channel and of tail half-charge; the latter has cylinder channel with axial symmetrical groove. In cross section of the star-shaped channel of the head half-charge minimal distance from a peak of ray to the point, where radius, passing through an arch of the head half-charge of maximal initial thickness, crosses the protective-fixing layer, is equal to 0.92…1.0 of initial thickness of a burning arch average to length of the tail half-charge. Length of axis symmetrical groove is 2.0…2.5 of length of cantilever section of the tail half-charge in the region of the front end.

EFFECT: increased reliability of solid fuel charge and reduced spread of power characteristics of engine.

2 dwg

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Authors

Povarov Sergej Aleksandrovich

Mel'Nik Gennadij Ivanovich

Shabalin Vladimir Mikhajlovich

Makarovets Nikolaj Aleksandrovich

Denezhkin Gennadij Alekseevich

Kaljuzhnyj Gennadij Vasil'Evich

Peturkin Dmitrij Mikhajlovich

Kashirkin Aleksandr Aleksandrovich

Erokhin Vladimir Evgen'Evich

Zakharov Oleg L'Vovich

Tregubov Viktor Ivanovich

Kutsenko Gennadij Vasil'Evich

Amarantov Georgij Nikolaevich

Nekrasov Valentin Ivanovich

Kovtun Viktor Evgen'Evich

Kolach Petr Kuz'Mich

Aljazhedinov Vadim Rashitovich

Dates

2010-06-10Published

2008-11-13Filed