UA61327U - Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen - Google Patents

Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen

Info

Publication number
UA61327U
UA61327U UAU201103136U UAU201103136U UA61327U UA 61327 U UA61327 U UA 61327U UA U201103136 U UAU201103136 U UA U201103136U UA U201103136 U UAU201103136 U UA U201103136U UA 61327 U UA61327 U UA 61327U
Authority
UA
Ukraine
Prior art keywords
tank
liquid oxygen
carrier rocket
missile system
aircraft missile
Prior art date
Application number
UAU201103136U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Константин Германович Алексеев
Александр Михайлович Комиссаров
Александр Васильевич Мокин
Галина Николаевна Никольская
Сергей Павлович Рожков
Original Assignee
Константин Германович Алексеев
Александр Михайлович Комиссаров
Мокин Андрей Александрович
Александр Васильевич Мокин
Галина Николаевна Никольская
Сергей Павлович Рожков
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 Константин Германович Алексеев, Александр Михайлович Комиссаров, Мокин Андрей Александрович, Александр Васильевич Мокин, Галина Николаевна Никольская, Сергей Павлович Рожков filed Critical Константин Германович Алексеев
Priority to UAU201103136U priority Critical patent/UA61327U/en
Publication of UA61327U publication Critical patent/UA61327U/en

Links

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  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

A method of filling a tank of a carrier rocket of aircraft missile system with liquid oxygen, in which filling of the tank of carrier rocket and a cryogenic tank is made with liquid oxygen under the temperature corresponding to its boiling point at normal atmospheric pressure. Temperature control of liquid oxygen in the tank of carrier rocket is carried out by initiating a process of boiling of liquid oxygen in the tank of carrier rocket and cryogenic tank by connecting the gas part of cryogenic tank to the atmosphere and use of change of atmospheric pressure outboard, which leads to overcooling liquid oxygen. The desired temperature of the liquid oxygen in the tank of carrier rocket is achieved by maintaining in it of required pressure value using an adjustable valve on the pipeline connecting the gas part of tank of carrier rocket and the cryogenic tank.
UAU201103136U 2011-03-17 2011-03-17 Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen UA61327U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201103136U UA61327U (en) 2011-03-17 2011-03-17 Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201103136U UA61327U (en) 2011-03-17 2011-03-17 Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen

Publications (1)

Publication Number Publication Date
UA61327U true UA61327U (en) 2011-07-11

Family

ID=50835583

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201103136U UA61327U (en) 2011-03-17 2011-03-17 Method of filling tank of carrier rocket of aircraft missile system with liquid oxygen

Country Status (1)

Country Link
UA (1) UA61327U (en)

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