RU2000111094A - LIQUID ROCKET MOTOR UNIT - Google Patents

LIQUID ROCKET MOTOR UNIT

Info

Publication number
RU2000111094A
RU2000111094A RU2000111094/06A RU2000111094A RU2000111094A RU 2000111094 A RU2000111094 A RU 2000111094A RU 2000111094/06 A RU2000111094/06 A RU 2000111094/06A RU 2000111094 A RU2000111094 A RU 2000111094A RU 2000111094 A RU2000111094 A RU 2000111094A
Authority
RU
Russia
Prior art keywords
motor unit
rocket motor
liquid rocket
tanks
fuel
Prior art date
Application number
RU2000111094/06A
Other languages
Russian (ru)
Other versions
RU2187010C2 (en
Inventor
Михаил Юрьевич Иванов
Руслан Эдуардович Катков
Николай Николаевич Тупицын
Original Assignee
Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева"
Filing date
Publication date
Application filed by Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" filed Critical Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева"
Priority to RU2000111094/06A priority Critical patent/RU2187010C2/en
Priority claimed from RU2000111094/06A external-priority patent/RU2187010C2/en
Publication of RU2000111094A publication Critical patent/RU2000111094A/en
Application granted granted Critical
Publication of RU2187010C2 publication Critical patent/RU2187010C2/en

Links

Claims (1)

Жидкостная ракетная двигательная установка, содержащая торообразные баки горючего и окислителя с заборными устройствами, двигатель, расположенный в свободном внутриторовом объеме, отличающаяся тем, что баки горючего и окислителя выполнены в виде сегментов одного полого тора, ограниченных по торцам поверхностями с ненулевой кривизной, являющимися днищами этих баков.A liquid-propellant rocket propulsion system containing toroidal fuel and oxidizer tanks with intake devices, an engine located in a free intra-second volume, characterized in that the fuel and oxidizer tanks are made in the form of segments of one hollow torus, bounded at the ends by surfaces with non-zero curvature, which are the bottoms of these tanks.
RU2000111094/06A 2000-05-03 2000-05-03 Liquid propellant rocket engine installation RU2187010C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000111094/06A RU2187010C2 (en) 2000-05-03 2000-05-03 Liquid propellant rocket engine installation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000111094/06A RU2187010C2 (en) 2000-05-03 2000-05-03 Liquid propellant rocket engine installation

Publications (2)

Publication Number Publication Date
RU2000111094A true RU2000111094A (en) 2002-04-20
RU2187010C2 RU2187010C2 (en) 2002-08-10

Family

ID=20234200

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000111094/06A RU2187010C2 (en) 2000-05-03 2000-05-03 Liquid propellant rocket engine installation

Country Status (1)

Country Link
RU (1) RU2187010C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2584045C2 (en) * 2014-03-03 2016-05-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Rocket booster and assembly method thereof

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