Long-Term Firing Tests of the Nozzles of Rocket Engines Made on the Basis of Carbon Composite Materials

A. M. Gubertov; V. V. Koshlakov; V. V. Mironov; V. R. Rubinskii; A. V. Pashutov; Ye. A. Antipov; N. A. Bratukhin; N. N. Volkov; L. I. Volkova; S. M. Tsatsuev; V. V. Tlevtsezhev

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Long-Term Firing Tests of the Nozzles of Rocket Engines Made on the Basis of Carbon Composite Materials

机译：基于碳复合材料的火箭发动机喷嘴的长期燃烧试验

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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 liq-uid-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.

机译：提出了对碳复合材料和液体推进剂火箭发动机喷嘴的相互作用，破坏和烧蚀的物理化学过程进行实验研究的结果。分析了复合材料制成的喷嘴与火箭发动机金属燃烧室在标准工作条件下的接合处的热应力状态。

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《Thermal engineering》 |2012年第14期|1068-1073|共6页
作者
A. M. Gubertov; V. V. Koshlakov; V. V. Mironov; V. R. Rubinskii; A. V. Pashutov; Ye. A. Antipov; N. A. Bratukhin; N. N. Volkov; L. I. Volkova; S. M. Tsatsuev; V. V. Tlevtsezhev;
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State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

JSC Chemical Automation Design Bureau, Voronezh;

JSC Central Research Institute for Special Machinery, Khot'kovo;

JSC Central Research Institute for Special Machinery, Khot'kovo;

JSC Chemical Automation Design Bureau, Voronezh;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

State Scientific Center, Federal State Unitary Enterprise "Keldysh Research Center, " Moscow;

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专利

1. LONG-RUN TESTING OF MODEL NOZZLE EXTENSIONS MADE OF A CARBON-CARBON COMPOSITE MATERIAL IN A LIQUID-PROPELLANT ROCKET ENGINE OPERATING ON HYDROGEN AND OXYGEN [J] . Anikin A. V., Berdov R. D., Volkov N. N., Journal of Applied Mechanics and Technical Physics . 2019,第1期

机译：在氢和氧作用下的液体火箭发动机中碳-碳复合材料制成的模型喷嘴延伸量的长期测试
2. LONG-RUN TESTING OF MODEL NOZZLE EXTENSIONS MADE OF A CARBON-CARBON COMPOSITE MATERIAL IN A LIQUID-PROPELLANT ROCKET ENGINE OPERATING ON HYDROGEN AND OXYGEN [J] . Anikin A. V., Berdov R. D., Volkov N. N., Journal of Applied Mechanics and Technical Physics . 2019,第1期

机译：在氢气和氧气上运行的液体推进式火箭发动机中由碳 - 碳复合材料制成的模型喷嘴延伸的长期测试
3. Network simulation of the rapid temperature changes in the composite nozzle wall of an experimental rocket engine during a ground firing test [J] . Francisco Alhama, Antonio Campo Applied thermal engineering: Design, processes, equipment, economics . 2003,第1期

机译：地面发射试验过程中实验火箭发动机复合喷嘴壁温度快速变化的网络模拟
4. Channel Wall Nozzle Manufacturing and Hot-Fire Testing using a Laser Wire Direct Closeout Technique for Liquid Rocket Engines [C] . Paul R. Gradl, Will Brandsmeier, Sandy E. Greene AIAA/SAE/ASEE joint propulsion conference;AIAA propulsion and energy forum . 2018

机译：使用液体火箭发动机的激光线直接封闭技术进行通道壁喷嘴制造和热火测试
5. Usage of vapor-grown carbon fiber composite with phenolic matrix in the space shuttle reusable solid rocket motor nozzle. [D] . Hill, Jeanene Renee. 1999

机译：气相生长的碳纤维复合材料与酚醛基质在航天飞机可重复使用的固体火箭发动机喷嘴中的使用。
6. A new technique for tensile testing of engineering materials and composites at high strain rates [O] . J. Zhou, A. Pellegrino, U. Heisserer, -1

机译：高应变率的工程材料和复合材料的拉伸测试一种新技术
7. The rocket nozzles made of carbon and carbon composite materials. [O] . Tateo HOSOMURA, Teruo SOFUE 1986

机译：火箭喷嘴由碳和碳复合材料制成。

Long-Term Firing Tests of the Nozzles of Rocket Engines Made on the Basis of Carbon Composite Materials

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