Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles

A. V. Kolychev; V. A. Kernozhitskii; M. V. Chernyshov

doi:10.3103/S1068799819040184

Thermionic Methods of Cooling for Thermostressed Elements of Advanced Reusable Launch Vehicles

作者: Kolychev A.V.¹, Kernozhitskii V.A.¹, Chernyshov M.V.¹
隶属关系:
1. Ustinov Baltic State Technical University “Voenmekh”
期: 卷 62, 编号 4 (2019)
页面: 669-674
栏目: 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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详细

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.