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Analyzing thermal state of the Buran orbital space vehicle structure in the areas of possible damages to its thermal protection elements
| Authors: Timoshenko V.P., Prosuntsov P.V., Reznik S.V. | Published: 10.06.2024 |
| Published in issue: #6(771)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: thermal protection, fibrous ceramics, felt substrate, thermal conductivity coefficient, thermal destruction, metal skin melting |
