UA97328U - The system of air temperature control of the head block of a rocket - Google Patents

The system of air temperature control of the head block of a rocket

Info

Publication number
UA97328U
UA97328U UAU201410061U UAU201410061U UA97328U UA 97328 U UA97328 U UA 97328U UA U201410061 U UAU201410061 U UA U201410061U UA U201410061 U UAU201410061 U UA U201410061U UA 97328 U UA97328 U UA 97328U
Authority
UA
Ukraine
Prior art keywords
air
rocket
temperature control
air temperature
head block
Prior art date
Application number
UAU201410061U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Andrii Anatoliiovych Isaiev
Andrii Serhiiovych Moisieiev
Andrii Oleksandrovych Mokin
Oleksandr Vasyliovych Mokin
Ivan Yuriiovych Tsipun
Serhii Ivanovych Yatsiuta
Original Assignee
Andrii Anatoliiovych Isaiev
Andrii Serhiiovych Moisieiev
Andrii Oleksandrovych Mokin
Oleksandr Vasyliovych Mokin
Ivan Yuriiovych Tsipun
Serhii Ivanovych Yatsiuta
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 Andrii Anatoliiovych Isaiev, Andrii Serhiiovych Moisieiev, Andrii Oleksandrovych Mokin, Oleksandr Vasyliovych Mokin, Ivan Yuriiovych Tsipun, Serhii Ivanovych Yatsiuta filed Critical Andrii Anatoliiovych Isaiev
Priority to UAU201410061U priority Critical patent/UA97328U/en
Publication of UA97328U publication Critical patent/UA97328U/en

Links

Landscapes

  • Air-Conditioning For Vehicles (AREA)

Abstract

Система повітряного термостатування головного блока ракети, містить джерело повітряного постачання, виконане у вигляді ресиверів стисненого повітря, трубопровід подавання з фільтром і керованою арматурою, котрий з'єднує джерело повітряного постачання з бортовим рознімним з'єднанням головного блока, охолоджувач повітря, насос, холодильну машину, електронагрівник, виконаний у вигляді теплоізольованого металевого корпусу з кришкою і трубчастими електронагрівачами, та пульт керування з датчиком температури. Ресивери стисненого повітря розділені зворотним клапаном на дві частини, котрі мають різну величину тиску повітря.The system of air conditioning of the main unit of the rocket, contains an air supply source, made in the form of compressed air receivers, a supply line with a filter and controlled fittings, which connects the air supply source with the onboard detachable connection of the main unit, air cooler, pump, chiller , an electric heater made in the form of a heat-insulated metal housing with a lid and tubular electric heaters, and a control panel with a temperature sensor. The compressed air receivers are divided by a non-return valve into two parts that have different values of air pressure.

UAU201410061U 2014-09-15 2014-09-15 The system of air temperature control of the head block of a rocket UA97328U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201410061U UA97328U (en) 2014-09-15 2014-09-15 The system of air temperature control of the head block of a rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201410061U UA97328U (en) 2014-09-15 2014-09-15 The system of air temperature control of the head block of a rocket

Publications (1)

Publication Number Publication Date
UA97328U true UA97328U (en) 2015-03-10

Family

ID=52990491

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201410061U UA97328U (en) 2014-09-15 2014-09-15 The system of air temperature control of the head block of a rocket

Country Status (1)

Country Link
UA (1) UA97328U (en)

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