RU2004101690A - ROCKET ACCELERATION UNIT - Google Patents

ROCKET ACCELERATION UNIT Download PDF

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Publication number
RU2004101690A
RU2004101690A RU2004101690/11A RU2004101690A RU2004101690A RU 2004101690 A RU2004101690 A RU 2004101690A RU 2004101690/11 A RU2004101690/11 A RU 2004101690/11A RU 2004101690 A RU2004101690 A RU 2004101690A RU 2004101690 A RU2004101690 A RU 2004101690A
Authority
RU
Russia
Prior art keywords
rocket
adapter
acceleration unit
tank
rocket acceleration
Prior art date
Application number
RU2004101690/11A
Other languages
Russian (ru)
Inventor
Владимир Владимирович Ерпылев (RU)
Владимир Владимирович Ерпылев
Александр Алексеевич Лобнев (RU)
Александр Алексеевич Лобнев
Михаил Викторович Рожков (RU)
Михаил Викторович Рожков
Original Assignee
Открытое акционернное общество "Ракетно-космическа корпораци "Энерги " им. С.П. Королева" (RU)
Открытое акционернное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева"
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 Открытое акционернное общество "Ракетно-космическа корпораци "Энерги " им. С.П. Королева" (RU), Открытое акционернное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" filed Critical Открытое акционернное общество "Ракетно-космическа корпораци "Энерги " им. С.П. Королева" (RU)
Priority to RU2004101690/11A priority Critical patent/RU2004101690A/en
Publication of RU2004101690A publication Critical patent/RU2004101690A/en

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  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Claims (1)

Ракетный разгонный блок, содержащий приборный отсек, бак окислителя, верхний переходник, межбаковый отсек, маршевый двигатель, бак горючего, средний переходник, нижний переходник, отличающийся тем, что для удержания отделяемых частей разъемных соединений от соударения с сопловым насадком маршевого двигателя применены тросы, которые одним концом закреплены к отделяемым частям разделяемых соединений, а другим - к корпусу нижнего переходника ракетного разгонного блока.The rocket booster block containing the instrument compartment, oxidizer tank, upper adapter, inter-tank compartment, main engine, fuel tank, middle adapter, lower adapter, characterized in that cables are used to hold the detachable parts of the detachable joints from impact with the nozzle nozzle of the sustainer engine one end is fixed to the detachable parts of the shared connections, and the other to the body of the lower adapter of the rocket overclocking unit.
RU2004101690/11A 2004-01-20 2004-01-20 ROCKET ACCELERATION UNIT RU2004101690A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004101690/11A RU2004101690A (en) 2004-01-20 2004-01-20 ROCKET ACCELERATION UNIT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004101690/11A RU2004101690A (en) 2004-01-20 2004-01-20 ROCKET ACCELERATION UNIT

Publications (1)

Publication Number Publication Date
RU2004101690A true RU2004101690A (en) 2005-06-20

Family

ID=35835618

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004101690/11A RU2004101690A (en) 2004-01-20 2004-01-20 ROCKET ACCELERATION UNIT

Country Status (1)

Country Link
RU (1) RU2004101690A (en)

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Legal Events

Date Code Title Description
FA91 Application withdrawn (on applicant's request)

Effective date: 20060301