Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles
- Авторы: Kolychev A.V.1, Kernozhitskii V.A.1, Chernyshov M.V.1
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Учреждения:
- Ustinov Baltic State Technical University “Voenmekh”
- Выпуск: Том 62, № 4 (2019)
- Страницы: 669-674
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/231183
- DOI: https://doi.org/10.3103/S1068799819040184
- ID: 231183
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Аннотация
The technology of thermionic thermal protection of thermostressed elements for aviation and space equipment is discussed. This technology is based on the thermionic emission phenomenon. Estimations of temperature decrease of the surface of thermostressed subsystems of reusable spacecraft and orbital launch vehicles at the thermionic thermal protection application are given.
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Об авторах
A. Kolychev
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Россия, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Kernozhitskii
Ustinov Baltic State Technical University “Voenmekh”
Автор, ответственный за переписку.
Email: vakern@mail.ru
Россия, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
M. Chernyshov
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Россия, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
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