Long-term firing tests of the nozzles of rocket engines made on the basis of carbon composite materials
| Autor: | N. N. Volkov, V. V. Mironov, V. V. Koshlakov, V. V. Tlevtsezhev, A. M. Gubertov, S. M. Tsatsuev, L. I. Volkova, N. A. Bratukhin, V. R. Rubinskii, A. V. Pashutov, Ye. A. Antipov |
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| Rok vydání: | 2012 |
| Předmět: |
Materials science
business.product_category integumentary system business.industry medicine.medical_treatment Nozzle Rocket engine nozzle Energy Engineering and Power Technology chemistry.chemical_element Ablation Nuclear Energy and Engineering Rocket chemistry medicine Rocket engine Composite material Combustion chamber business Carbon |
| Zdroj: | Thermal Engineering. 59:1068-1073 |
| ISSN: | 1555-6301 0040-6015 |
| DOI: | 10.1134/s0040601512140042 |
| Popis: | The results of the experimental investigation of the physico-chemical processes of interaction, destruction, and ablation of carbon composite materials and oxidation-protective coatings of nozzles of liquid-propellant rocket engines are presented. The thermally-stressed state of the joint between the nozzle made of composite material and the metallic combustion chamber of the rocket engine under standard operating conditions have been analyzed. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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