Email this article Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles
- Authors: Kolychev A.V.1, Kernozhitskii V.A.1, Chernyshov M.V.1
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Affiliations:
- Ustinov Baltic State Technical University “Voenmekh”
- Issue: Vol 62, No 4 (2019)
- Pages: 669-674
- Section: 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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Abstract
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.
About the authors
A. V. Kolychev
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
V. A. Kernozhitskii
Ustinov Baltic State Technical University “Voenmekh”
Author for correspondence.
Email: vakern@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
M. V. Chernyshov
Ustinov Baltic State Technical University “Voenmekh”
Email: vakern@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
