Show metadata Hide metadata

(19)

(11)

2 197 629

(13)

(51)

IPC

(21) (22)

Application

2001107629/06, 2001-03-26

(24)

Start date

2001-03-26

(22)

Actual filing date

2001-03-26

(45)

Published

2003-01-27

(72)

Inventor

Bakhmutov A.A.Bukanov V.T.Klepikov I.A.Miroshkin V.V.Prishchepa V.I.Romasenko T.Ja.

(73)

Holder

Bakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKlepikov Igor' AlekseevichMiroshkin Vjacheslav Vasil'EvichPrishchepa Vladimir IosifovichRomasenko Tat'Jana Jakovlevna

METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF FUEL AND OXYGEN OXIDIZER AND LIQUID-PROPELLANT ROCKET ENGINE FOR IMPLEMENTING SAID METHOD Russian patent published in 2003 - IPC

Abstract RU 2197629 C2

FIELD: rocketry. SUBSTANCE: according to proposed method of operation of liquidpropellant rocket engine with turbopump delivery of cryogenic propellant on basis of oxygen oxidizer and fuel, recovering gas, after generation of vapor, is used directly for afterburning in chamber with remaining part of fuel. Liquid propellant rocket engine implementing proposed method employs gas generator designed for generating recovering gas being connected directly to nozzle head of chamber. EFFECT: increased efficiency of liquid-propellant rocket engine by increasing specific thrust pulse. 5 cl, 3 dwg

Similar patents RU2197629C2

Title	Year	Author	Number
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF OXYGEN OXIDIZER AND HYDROCARBON FUEL AND LIQUID- PROPELLANT ROCKET ENGINE IMPLEMENTING SAID METHOD	2001	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I. Romasenko T.Ja.	RU2197628C2
LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT	2001	Bakhmutov A.A. Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I. Romasenko T.Ja.	RU2202703C2
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
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH CLOSED STEAM-LIQUID CONTOUR IN TURBOPUMP DELIVERY SYSTEM	2002	Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I.	RU2211938C1
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH VAPOR-LIQUID LOOP IN PROPELLANT TURBOPUMP DELIVERY SYSTEM	2003	Bukanov V.T. Klepikov I.A. Miroshkin V.V. Prishchepa V.I.	RU2238424C1
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
ENGINE FOR LIQUID-PROPELLANT ROCKET POWER PLANT	1996	Bakhmutov Arkadij Alekseevich Bukanov Vladislav Timofeevich Klepikov Igor' Alekseevich Prishchepa Vladimir Iosifovich	RU2119081C1
TURBO-PUMP SUPPLY SYSTEM FOR LIQUID-PROPELLANT ROCKET ENGINE	2002	Bakhmutov A.A. Bukanov V.T. Kanalin Ju.I. Klepikov I.A. Miroshkin V.V. Prishchepa V.I.	RU2246023C2
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

RU 2 197 629 C2

Authors

Bakhmutov A.A.

Bukanov V.T.

Klepikov I.A.

Miroshkin V.V.

Prishchepa V.I.

Romasenko T.Ja.

Dates

2003-01-27—Published

2001-03-26—Filed