ROCKET CARRIAGE WITH CONTROLLED VECTOR OF THRUST Russian patent published in 2020 - IPC F42B35/00 F41F3/04 G01M7/08 G01M15/00 F02K9/96 

Abstract RU 2739546 C1

FIELD: test equipment.

SUBSTANCE: invention relates to test equipment, specifically to equipment for high-speed track tests, and can be used for acceleration of test objects on rocket track. Rocket carriage comprises bearing platform installed on pylons resting on support-and-guide shoes, located on it lodgments for installation of tested product and rocket engine, elements of braking system and rear fender. Support for installation of rocket engine is made with possibility of controlled rotation relative to horizontal axis perpendicular to direction of carriage movement, and anti-wing is configured to adjust angle of attack, as well as vertical plane-parallel movement relative to platform and is equipped with elements of rocket engine lodge turn control elements. Anti-wing can be equipped with elements of mechanization.

EFFECT: invention allows stabilization and maintenance of constant speed of rail carriage motion at preset distance of movement.

1 cl, 3 dwg

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RU 2 739 546 C1

Authors

Koltunov Vladimir Valentinovich

Vatutin Nikolaj Mikhajlovich

Fursov Yurij Serafimovich

Zaborovskij Aleksandr Dmitrievich

Lomakin Evgenij Aleksandrovich

Neudakhin Denis Dmitrievich

Zelenov Vladimir Vladimirovich

Dates

2020-12-25Published

2020-06-25Filed