RU2004107039A - LIQUID ROCKET ENGINE - Google Patents

LIQUID ROCKET ENGINE Download PDF

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Publication number
RU2004107039A
RU2004107039A RU2004107039/06A RU2004107039A RU2004107039A RU 2004107039 A RU2004107039 A RU 2004107039A RU 2004107039/06 A RU2004107039/06 A RU 2004107039/06A RU 2004107039 A RU2004107039 A RU 2004107039A RU 2004107039 A RU2004107039 A RU 2004107039A
Authority
RU
Russia
Prior art keywords
rocket engine
liquid rocket
liquid
chamber
liquid curtain
Prior art date
Application number
RU2004107039/06A
Other languages
Russian (ru)
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 Министерства обороны РФ (RU)
Военно-космическая академия им. А.Ф. Можайского Министерства 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 Министерства обороны РФ (RU), Военно-космическая академия им. А.Ф. Можайского Министерства обороны РФ filed Critical Военно-космическа академи им. А.Ф. Можайского Министерства обороны РФ (RU)
Priority to RU2004107039/06A priority Critical patent/RU2004107039A/en
Publication of RU2004107039A publication Critical patent/RU2004107039A/en

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  • Toys (AREA)
  • Engine Equipment That Uses Special Cycles (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 в линии подачи горючего на жидкостную завесу установлен регулятор расхода.A liquid rocket engine containing a chamber with a regenerative cooling system and a belt of a liquid curtain, a turbopump system for supplying components to the chamber and a gas generator, a control system with a draft regulator and a ratio control component, characterized in that a flow regulator is installed in the fuel supply line to the liquid curtain.
RU2004107039/06A 2004-03-09 2004-03-09 LIQUID ROCKET ENGINE RU2004107039A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004107039/06A RU2004107039A (en) 2004-03-09 2004-03-09 LIQUID ROCKET ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004107039/06A RU2004107039A (en) 2004-03-09 2004-03-09 LIQUID ROCKET ENGINE

Publications (1)

Publication Number Publication Date
RU2004107039A true RU2004107039A (en) 2005-09-27

Family

ID=35849537

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004107039/06A RU2004107039A (en) 2004-03-09 2004-03-09 LIQUID ROCKET ENGINE

Country Status (1)

Country Link
RU (1) RU2004107039A (en)

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20060607