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RU2004116170A - INTERBORNE VEHICLE VEHICLES - Google Patents

INTERBORNE VEHICLE VEHICLES Download PDF

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Publication number
RU2004116170A
RU2004116170A RU2004116170/11A RU2004116170A RU2004116170A RU 2004116170 A RU2004116170 A RU 2004116170A RU 2004116170/11 A RU2004116170/11 A RU 2004116170/11A RU 2004116170 A RU2004116170 A RU 2004116170A RU 2004116170 A RU2004116170 A RU 2004116170A
Authority
RU
Russia
Prior art keywords
stage
hose
fuel
compressed gas
interborne
Prior art date
Application number
RU2004116170/11A
Other languages
Russian (ru)
Inventor
Николай Федорович Аверкиев (RU)
Николай Федорович Аверкиев
В чеслав Викторович Салов (RU)
Вячеслав Викторович Салов
Михаил Васильевич Ведерников (RU)
Михаил Васильевич Ведерников
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 RU2004116170/11A priority Critical patent/RU2004116170A/en
Publication of RU2004116170A publication Critical patent/RU2004116170A/en

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  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Claims (1)

Межорбитальный транспортный летательный аппарат, содержащий емкости для транспортировки топлива, насос для перекачки топлива, систему ориентации и стабилизации, устройство стыковки со ступенью ракеты-носителя, двигательную установку, кран-ферму со шлангом, один конец которого герметично соединен с емкостью для транспортировки топлива, на другом конце установлен стыковочный узел, обеспечивающий герметичную стыковку шланга и сливного отверстия ступени ракеты-носителя, отличающийся тем, что для дозаправки топливом, оставшимся в ступенях ракет-носителей в конце активного участка полета, дополнительно включают емкости со сжатым газом и проходящую внутри шланга систему подвода сжатого газа, предназначенную для открытия сливного клапана ступени ракеты-носителя.An interorbital transport aircraft containing fuel transportation containers, a fuel transfer pump, an orientation and stabilization system, a docking device with a launch vehicle stage, a propulsion system, a crane farm with a hose, one end of which is hermetically connected to the fuel transportation container, on at the other end there is a docking unit, which provides a tight joint of the hose and the drain hole of the launch vehicle stage, characterized in that for refueling with the fuel remaining in the stage x boosters at the end of the active portion of the flight, further include a compressed gas container and extending inside the hose compressed gas supply system for opening the drain valve stage of the carrier rocket.
RU2004116170/11A 2004-05-27 2004-05-27 INTERBORNE VEHICLE VEHICLES RU2004116170A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004116170/11A RU2004116170A (en) 2004-05-27 2004-05-27 INTERBORNE VEHICLE VEHICLES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004116170/11A RU2004116170A (en) 2004-05-27 2004-05-27 INTERBORNE VEHICLE VEHICLES

Publications (1)

Publication Number Publication Date
RU2004116170A true RU2004116170A (en) 2005-11-10

Family

ID=35865095

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004116170/11A RU2004116170A (en) 2004-05-27 2004-05-27 INTERBORNE VEHICLE VEHICLES

Country Status (1)

Country Link
RU (1) RU2004116170A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2607912C2 (en) * 2007-03-09 2017-01-11 Макдоналд Деттуилер энд Ассошиэйтс Инк. System and method of satellites refueling

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2607912C2 (en) * 2007-03-09 2017-01-11 Макдоналд Деттуилер энд Ассошиэйтс Инк. System and method of satellites refueling

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Legal Events

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

Effective date: 20051121

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