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2 638 705

(13)

(51)

IPC

F02K9/42(2006-01-01)

(21) (22)

Application

2016119795, 2016-05-23

(24)

Start date

2016-05-23

(22)

Actual filing date

2016-05-23

(45)

Published

2017-12-15

(72)

Inventor

Ilin Aleksandr MikhajlovichMatveev Anton MikhajlovichDzis-Vojnarovskij Nikolaj NikolaevichSuvorov Andrej Valerevich

(73)

Holder

Obshchestvo S Ogranichennoj Otvetstvennostyu Indastrial"

LIQUID MISCELLANEOUS ENGINE WITH PERFECT PNEUMON PUMP UNIT Russian patent published in 2017 - IPC F02K9/42

Abstract RU 2638705 C1

FIELD: engines and pumps.

SUBSTANCE: invention can be used in the development of a launch vehicle (LV) for light loads. Liquid rocket engine (LRE) includes the combustion chamber, four pneumatic pump units for feeding fuel and oxidizer, a tank with high pressure helium, a tank with liquid methane, with each pneumatic pump unit containing two outlets for evacuation of the gaseous and liquid components. Gaseous components of methane and oxygen are diverted to the combustion control chambers for subsequent afterburning.

EFFECT: reducing the mass of the liquid rocket engine and increasing its efficiency, simplifying the design of the liquid rocket engine.

1 dwg

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RU 2 638 705 C1

Authors

Ilin Aleksandr Mikhajlovich

Matveev Anton Mikhajlovich

Dzis-Vojnarovskij Nikolaj Nikolaevich

Suvorov Andrej Valerevich

Dates

2017-12-15—Published

2016-05-23—Filed