UA77401U - Method of filling with liquid oxygen of tank of carrier rocket of aviation missile system - Google Patents

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

Info

Publication number
UA77401U
UA77401U UAU201209831U UAU201209831U UA77401U UA 77401 U UA77401 U UA 77401U UA U201209831 U UAU201209831 U UA U201209831U UA U201209831 U UAU201209831 U UA U201209831U UA 77401 U UA77401 U UA 77401U
Authority
UA
Ukraine
Prior art keywords
tank
carrier rocket
cryogenic
liquid oxygen
filling
Prior art date
Application number
UAU201209831U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Николай Дмитриевич Алехин
Ирина Николаевна Манойленко
Андрей Александрович Мокин
Александр Васильевич Мокин
Михаил Николаевич Сыровец
Сергей Александрович Юрченко
Original Assignee
Николай Дмитриевич Алехин
Ирина Николаевна Манойленко
Андрей Александрович Мокин
Александр Васильевич Мокин
Михаил Николаевич Сыровец
Сергей Александрович Юрченко
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 Николай Дмитриевич Алехин, Ирина Николаевна Манойленко, Андрей Александрович Мокин, Александр Васильевич Мокин, Михаил Николаевич Сыровец, Сергей Александрович Юрченко filed Critical Николай Дмитриевич Алехин
Priority to UAU201209831U priority Critical patent/UA77401U/en
Publication of UA77401U publication Critical patent/UA77401U/en

Links

Landscapes

  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

A method of filling with liquid oxygen of a tank of a carrier rocket of an aviation missile system includes filling with liquid oxygen of the tank of the carrier rocket to a predetermined level and with cryogenic component of a cryogenic tank, which are located in the cargo compartment of the aircraft, and temperature control of the liquid oxygen in the tank of carrier rocket during flight of an aircraft up to landing at a given height using a cryogenic tanks with cryogenic component circulating through the tank of carrier rocket, when connecting the gas part of the tank to atmosphere. As a cryogenic component in a cryogenic tank a liquid nitrogen is used with initial temperature corresponding to its boiling point at normal atmospheric pressure.
UAU201209831U 2012-08-14 2012-08-14 Method of filling with liquid oxygen of tank of carrier rocket of aviation missile system UA77401U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201209831U UA77401U (en) 2012-08-14 2012-08-14 Method of filling with liquid oxygen of tank of carrier rocket of aviation missile system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201209831U UA77401U (en) 2012-08-14 2012-08-14 Method of filling with liquid oxygen of tank of carrier rocket of aviation missile system

Publications (1)

Publication Number Publication Date
UA77401U true UA77401U (en) 2013-02-11

Family

ID=51587015

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201209831U UA77401U (en) 2012-08-14 2012-08-14 Method of filling with liquid oxygen of tank of carrier rocket of aviation missile system

Country Status (1)

Country Link
UA (1) UA77401U (en)

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