Show metadata Hide metadata

(19)

(11)

2 156 874

(13)

(51)

IPC

(21) (22)

Application

99112443/06, 1999-06-09

(24)

Start date

1999-06-09

(22)

Actual filing date

1999-06-09

(45)

Published

2000-09-27

(72)

Inventor

Bakhmutov A.A.Bukanov V.T.Klepikov I.A.Prishchepa V.I.

(73)

Holder

Bakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKlepikov Igor' AlekseevichPrishchepa Vladimir Iosifovich

CONTROLLABLE LIQUID-PROPELLANT MULTI-CHAMBER ROCKET VEHICLE Russian patent published in 2000 - IPC

Abstract RU 2156874 C1

FIELD: rocketry. SUBSTANCE: proposed rocket vehicle has case with oxidizer and fuel tanks, power plant consisting of several reaction chambers, single-axle articulated suspensions for mounting the chambers on rocket vehicle for their turn required for control of flight and servo units for performing such turns. Axle of articulated suspension is perpendicular to plane passing through longitudinal axes of vehicle and respective chamber, thus ensuring control of flight in pitch and yaw. Vehicle is provided with reaction nozzles for roll control. EFFECT: possibility of performing controllable flight at partial disconnection of reaction chambers. 2 dwg

Similar patents RU2156874C1

Title	Year	Author	Number
POWER PLANT OF CONTROLLED LIQUID-PROPELLANT ROCKET VEHICLE	1999	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Prishchepa V.I.	RU2163304C1
ENGINE FOR LIQUID-PROPELLANT ROCKET POWER PLANT	1996	Bakhmutov Arkadij Alekseevich Bukanov Vladislav Timofeevich Klepikov Igor' Alekseevich Prishchepa Vladimir Iosifovich	RU2119081C1
AIRCRAFT ENGINE UNIT	1995	Bakhmutov Arkadij Alekseevich Klepikov Igor' Alekseevich Prishchepa Vladimir Iosifovich	RU2089743C1
MULTISTAGE ROCKET	1994	Bakhmutov Arkadij Alekseevich Klepikov Igor' Alekseevich Prishchepa Vladimir Iosifovich	RU2088787C1
METHOD OF STARTING LIQUID ROCKET ENGINE AND LIQUID ROCKET ENGINE	1994	Klepikov Igor' Alekseevich Bakhmutov Arkadij Alekseevich Bukanov Vladislav Timofeevich Kanalin Jurij Ivanovich Prishchepa Vladimir Iosifovich	RU2084677C1
THROTTLEABLE OXYGEN-HYDROCARBON LIQUID-PROPELLANT ROCKET ENGINE WITH AFTERBURNING OF RECOVERY GAS	2002	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I.	RU2238423C2
MULTI-STAGE ROCKET	1994	Bakhmutov Arkadij Alekseevich Klepikov Igor' Alekseevich Obukhov Nikolaj Aleksandrovich Mogilenko Vladimir Ivanovich	RU2086795C1
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE AT TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT	1999	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I. Romasenko T.Ja.	RU2166661C1
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF OXYGEN-METHANE PROPELLANT	2001	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I.	RU2209993C2
HINGED SUSPENSION FOR MOUNTING REACTION CHAMBER ON FLYING VEHICLE	1995	Bakhmutov Arkadij Alekseevich Klepikov Igor' Alekseevich	RU2090773C1

RU 2 156 874 C1

Authors

Bakhmutov A.A.

Bukanov V.T.

Klepikov I.A.

Prishchepa V.I.

Dates

2000-09-27—Published

1999-06-09—Filed