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2 289 034

(13)

(51)

IPC

F02K9/36(2006-01-01)

(21) (22)

Application

2005115682/06, 2005-05-23

(24)

Start date

2005-05-23

(22)

Actual filing date

2005-05-23

(45)

Published

2006-12-10

(72)

Inventor

Aref'Ev Vadim SergeevichZagitov Azgar MirkhatipovichArtamonov Sergej ValerievichDenezhkin Gennadij AlekseevichDruzhinin Vladimir Evgen'EvichMakartsov Andrej MikhajlovichMakarovets Nikolaj AleksandrovichManchuk Boris Vladimirovich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Institut Polimernykh Materialov"Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

ROCKET ENGINE OF IMPULSE VERNIER UNIT Russian patent published in 2006 - IPC F02K9/36

Abstract RU 2289034 C1

FIELD: rocketry.

SUBSTANCE: invention relates to impulse-type rocket engines with small time of operation and considerable loads acting onto charge. Proposed rocket engine of impulse vernier unit has body, solid-propellant change in form of charge tube cluster, igniter arranged in head part of engine, and nozzle. Tubes are held on carrying plate in head part of engine by cap of cylindrical pins connected pins connected with channel of charge tubes. Odd number of parallel slots is made on carrying plate for arrangement of pins in opposite directions.

EFFECT: improved reliability and mass perfection of vernier unit.

4 cl, 3 dwg

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RU 2 289 034 C1

Authors

Aref'Ev Vadim Sergeevich

Zagitov Azgar Mirkhatipovich

Artamonov Sergej Valerievich

Denezhkin Gennadij Alekseevich

Druzhinin Vladimir Evgen'Evich

Makartsov Andrej Mikhajlovich

Makarovets Nikolaj Aleksandrovich

Manchuk Boris Vladimirovich

Dates

2006-12-10—Published

2005-05-23—Filed