Мақаланы E-mail арқылы жіберу Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles
- Авторлар: Kolychev A.V.1, Kernozhitskii V.A.1, Chernyshov M.V.1
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Мекемелер:
- Ustinov Baltic State Technical University “Voenmekh”
- Шығарылым: Том 62, № 4 (2019)
- Беттер: 669-674
- Бөлім: 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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Авторлар туралы
A. Kolychev
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Ресей, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Kernozhitskii
Ustinov Baltic State Technical University “Voenmekh”
Хат алмасуға жауапты Автор.
Email: vakern@mail.ru
Ресей, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
M. Chernyshov
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Ресей, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
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