RU2004107038A - LIQUID ROCKET ENGINE - Google Patents

LIQUID ROCKET ENGINE Download PDF

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Publication number
RU2004107038A
RU2004107038A RU2004107038/06A RU2004107038A RU2004107038A RU 2004107038 A RU2004107038 A RU 2004107038A RU 2004107038/06 A RU2004107038/06 A RU 2004107038/06A RU 2004107038 A RU2004107038 A RU 2004107038A RU 2004107038 A RU2004107038 A RU 2004107038A
Authority
RU
Russia
Prior art keywords
chamber
rocket engine
liquid rocket
cooling
regulator
Prior art date
Application number
RU2004107038/06A
Other languages
Russian (ru)
Other versions
RU2279563C2 (en
Inventor
ев Борис Васильевич Бел (RU)
Борис Васильевич Беляев
Захар Сергеевич Великий (RU)
Захар Сергеевич Великий
Дмитрий Владимирович Ильич (RU)
Дмитрий Владимирович Ильич
Александр Владимирович Кузьминых (RU)
Александр Владимирович Кузьминых
ев Иван Борисович Бел (RU)
Иван Борисович Беляев
Original Assignee
Военно-космическа академи им. А.Ф. Можайского Министерство Обороны РФ (RU)
Военно-космическая академия им. А.Ф. Можайского Министерство Обороны РФ
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Военно-космическа академи им. А.Ф. Можайского Министерство Обороны РФ (RU), Военно-космическая академия им. А.Ф. Можайского Министерство Обороны РФ filed Critical Военно-космическа академи им. А.Ф. Можайского Министерство Обороны РФ (RU)
Priority to RU2004107038/06A priority Critical patent/RU2279563C2/en
Publication of RU2004107038A publication Critical patent/RU2004107038A/en
Application granted granted Critical
Publication of RU2279563C2 publication Critical patent/RU2279563C2/en

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  • Testing Of Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Claims (1)

Жидкостный ракетный двигатель, содержащий камеру с регенеративной системой охлаждения и поясом жидкостной завесы, турбонасосную систему подачи компонентов в камеру и газогенератор, систему управления с регулятором тяги и регулятором соотношения компонентов, отличающийся тем, что параллельно линии горючего на охлаждение камеры установлена обводная магистраль с регулятором расхода, перепускающая часть горючего в камеру сгорания, минуя тракт охлаждения.A liquid-propellant rocket engine comprising a chamber with a regenerative cooling system and a liquid curtain belt, a turbopump system for supplying components to the chamber and a gas generator, a control system with a draft regulator and a ratio regulator, characterized in that a bypass line with a flow regulator is installed parallel to the fuel line for cooling the chamber , passing part of the fuel into the combustion chamber, bypassing the cooling path.
RU2004107038/06A 2004-03-09 2004-03-09 Liquid-propellant rocket engine RU2279563C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004107038/06A RU2279563C2 (en) 2004-03-09 2004-03-09 Liquid-propellant rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004107038/06A RU2279563C2 (en) 2004-03-09 2004-03-09 Liquid-propellant rocket engine

Publications (2)

Publication Number Publication Date
RU2004107038A true RU2004107038A (en) 2005-09-27
RU2279563C2 RU2279563C2 (en) 2006-07-10

Family

ID=35849536

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004107038/06A RU2279563C2 (en) 2004-03-09 2004-03-09 Liquid-propellant rocket engine

Country Status (1)

Country Link
RU (1) RU2279563C2 (en)

Also Published As

Publication number Publication date
RU2279563C2 (en) 2006-07-10

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Legal Events

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MM4A The patent is invalid due to non-payment of fees