Enviar artigo por via de e-mail Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles
- Autores: Kolychev A.1, Kernozhitskii V.1, Chernyshov M.1
-
Afiliações:
- Ustinov Baltic State Technical University “Voenmekh”
- Edição: Volume 62, Nº 4 (2019)
- Páginas: 669-674
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/231183
- DOI: https://doi.org/10.3103/S1068799819040184
- ID: 231183
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
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.
Palavras-chave
Sobre autores
A. Kolychev
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Rússia, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. Kernozhitskii
Ustinov Baltic State Technical University “Voenmekh”
Autor responsável pela correspondência
Email: vakern@mail.ru
Rússia, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
M. Chernyshov
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Rússia, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
