Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Рустем Юсуфович Турна"'
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 2, Pp 36-51 (2021)
The progress of space technology is leading to more and more energy-equipped spacecraft. The International Space Station already has the capacity of solar panels of more than 100 kW. Autonomous spacecrafts and satellites (including stationary ones) h
Externí odkaz:
https://doaj.org/article/c1e8e72bfa484b3b968382cb053ac2f5
Autor:
Рустем Юсуфович Турна
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 1, Pp 31-46 (2021)
For spacecraft (SC) with power unit capacity more than 4 ... 6 kW promising construction of thermal control system (TCS) based on two-phase mechanically pumped loops (2PMPL). The development of 2PMPL has been carried out quite intensively since the e
Externí odkaz:
https://doaj.org/article/69c8c9d7866b44b098f1a9db221d2c6d
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 4, Pp 12-21 (2020)
It is advisable to use two-phase heat transfer circuits (TPC) on spacecraft with high heat release in thermal control systems (TCS). TPC has many advantages over single-phase heat transfer loops. In such circuits, heat is accumulated and transferred
Externí odkaz:
https://doaj.org/article/5dfff7e80a844f988959b6a9ced240d9
Autor:
Геннадий Александрович Горбенко, Рустем Юсуфович Турна, Роман Сергеевич Орлов, Евгений Эдуардович Роговой
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 8, Pp 27-33 (2020)
In the manufacture of wicks for capillary transport of coolant in various heat transfer devices such as heat pipes, capillary pumped loop, accumulators with thermal regulation, evaporative heat exchangers, heat sinks, etc., capillary porous structure
Externí odkaz:
https://doaj.org/article/d32f565071184b1ba6016501409d08b0
Autor:
Артем Михайлович Годунов, Евгений Эдуардович Роговой, Роман Сергеевич Орлов, Рустем Юсуфович Турна
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 7, Pp 31-38 (2019)
Technical progress entails the use of more powerful equipment on satellites. In connection with the growth of heat generation onboard the spacecraft, the task is to develop thermal control systems based on two-phase mechanically pumped fluid loop (2P
Externí odkaz:
https://doaj.org/article/157e5dd8891742d08ba022c14ffc5243
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 8, Pp 10-15 (2019)
In the modern world with the increasing power of spacecraft heat dissipation, the need has arisen to use efficient heat removal systems with two-phase heat transfer contours. Their advantages are determined by the fact that they can carry a much larg
Externí odkaz:
https://doaj.org/article/7bf5767382a8471d976211278dab6cdf
Autor:
Павел Григорьевич Гакал, Геннадий Александрович Горбенко, Эдем Русланович Решитов, Рустем Юсуфович Турна
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 8, Pp 24-29 (2018)
The world trend in the development of space vehicles is the expansion of their functionality, which leads to an increase in the power consumption, most of which is allocated in the elements of spacecraft equipment in the form of heat. To remove heat
Externí odkaz:
https://doaj.org/article/43f0ae8db8b74d30810163fe1601d44c