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(19)

(11)

2 489 329

(13)

(51)

IPC

B64G1/24(2006-01-01)

F42B15/00(2006-01-01)

F42B10/26(2006-01-01)

(21) (22)

Application

2012111451/11, 2012-03-27

(24)

Start date

2012-03-27

(22)

Actual filing date

2012-03-27

(45)

Published

2013-08-10

(72)

Inventor

Al'Tshuler Aleksandr SholomovichLobanov Vladimir Anatol'EvichKitina Irina Aleksandrovna

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Kosmicheskij Nauchno-Proizvodstvennyj Tsentr Imeni M.V. Khrunicheva"

CARRIER ROCKET Russian patent published in 2013 - IPC B64G1/24 F42B15/00 F42B10/26

Abstract RU 2489329 C1

FIELD: transport.

SUBSTANCE: invention relates to aerospace engineering, particularly, to means for placing spaceships in orbit. Carrier rocket comprises one sustainer engine at gimbal suspension and jettisonable first stage. Said first stage comprises aerodynamic roll system with hydraulic servo drives at maximum ram pressure in orbiting of carrier rocket. Said hydraulic servo drives are equipped with fluid-driven locks for automatic locking in preset position with shutdown sustainer and no pressure in said hydraulic servo drives of aerodynamic roll system arranged at rocket carrier jettisonable first stage nose.

EFFECT: decreased scatter of first stage drop points.

5 dwg

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RU 2 489 329 C1

Authors

Al'Tshuler Aleksandr Sholomovich

Lobanov Vladimir Anatol'Evich

Kitina Irina Aleksandrovna

Dates

2013-08-10—Published

2012-03-27—Filed