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2 399 782

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(51)

IPC

F02K9/36(2006-01-01)

(21) (22)

Application

2009108896/06, 2009-03-10

(24)

Start date

2009-03-10

(22)

Actual filing date

2009-03-10

(45)

Published

2010-09-20

(72)

Inventor

Osjaev Oleg Gennad'EvichOstapenko Aleksandr VladimirovichTaturin Jurij AleksandrovichSakhabudinov Roman VladislavovichSizov Igor' MikhajlovichMomotov Mikhail Andreevich

(73)

Holder

Gosudarstvennoe Obrazovatel'Noe Uchrezhdenie Vysshego Professional'Nogo Obrazovanija Voennyj Institut Raketnykh Vojsk Imeni Glavnogo Marshala Artillerii M.I. Nedelina"

FACILITY FOR REFUELLING SOLID-PROPELLANT CHARGE IN ROCKET ENGINE OF SOLID PROPELLANT Russian patent published in 2010 - IPC F02K9/36

Abstract RU 2399782 C1

FIELD: machine building.

SUBSTANCE: facility for refuelling solid-propellant charge in rocket engine of solid propellant consists of vertical plates with cross accessories arranged along combustion chamber of engine. The vertical plates are made out of aluminium-magnesium alloy and ensure protection of the solid-propellant charge from deformation of continuous static loads.

EFFECT: reduction of static loads effecting structure of rocket engine during continuous operation without essential deterioration of tactic-technical characteristics of rockets of strategic purpose.

2 dwg

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RU 2 399 782 C1

Authors

Osjaev Oleg Gennad'Evich

Ostapenko Aleksandr Vladimirovich

Taturin Jurij Aleksandrovich

Sakhabudinov Roman Vladislavovich

Sizov Igor' Mikhajlovich

Momotov Mikhail Andreevich

Dates

2010-09-20—Published

2009-03-10—Filed