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DESIGN AND DEVELOPMENT OF REFRACTORY CERAMIC LINING FOR COMBUSTION CHAMBER OF UNCOOLED ROCKET MOTOR

机译：无火箭发动机燃烧室耐火陶瓷衬里的设计与开发

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摘要

To present a new tile design and data upon its development for use in uncooled rocket motor liners.

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作者
Dwight G. Bennett; Robert F. Kimpel;
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年度 1949
页码 1-12
总页数 12
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. AN ANALYSIS OF THE EFFICIENCY GAINED WITH REPLACEMENT OF THE TRADITIONAL LINING OF BELL AND CHAMBER METALLURGICAL FURNACES BY LINING MADE OF REFRACTORY CERAMIC FIBER [J] . K. M. Mikhalev Refractories and Industrial Ceramics . 2010,第5期

机译：难熔陶瓷纤维衬里替代钟形和冶金冶金炉传统衬里的效率分析
2. Corrosion, current forms of damage corrosion of membrane walls in the combustion chamber through thermo-mechanical stress on the refractory lining on lines 1 to 3 of the Schwandorf Refuse-Fired power plant [J] . J. Kruger, J. Drexler VGB KraftwerksTechnik . 1998,第11期

机译：Schwandorf垃圾焚烧发电厂1号线至3号线耐火炉衬上的热机械应力腐蚀产生的当前形式的燃烧室膜壁腐蚀腐蚀
3. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors [J] . Emelyanov V. N., Teterina I. V., Volkov K. N., Acta astronautica . 2017,第JUNa期

机译：固体火箭发动机燃烧室中的压力振荡和工作过程的不稳定性
4. DESIGN AND DEVELOPMENT APPROACH FOR GAS TURBINE COMBUSTION CHAMBERS MADE OF OXIDE CERAMIC MATRIX COMPOSITES [C] . Ralf Knoche, Erich Werth, Markus Weth, International Conference on Advanced Ceramics and Composites;ICACC . 2011

机译：氧化陶瓷基复合材料燃气轮机燃烧室的设计与开发方法
5. INVESTIGATION OF COMBUSTION CHARACTERISTICS OF A HIGH CHAMBER PRESSURE ROCKET MOTOR. [D] . CARPENTER, THOMAS WILLIAM. 1969

机译：高腔压力火箭发动机燃烧特性的研究。
6. Transformation of Combustion Nanocatalysts inside Solid Rocket Motor under Various Pressures [O] . Jun-Qiang Li, Linlin Liu, Xiaolong Fu, 2019

机译：固体火箭发动机内燃烧纳米催化剂在不同压力下的转化
7. Pressure oscillations and instability of working processes in the combustion chambers of solid rocket motors [O] . Emelyanov V.N., Teterina I.V., Volkov K.N., 2017

机译：固体火箭发动机燃烧室内的压力振荡和工作过程的不稳定性
8. Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development of an Optimized Design [R] . Wadel, Mary F. 1998

机译：火箭燃烧室高纵横比冷却通道设计的比较及优化设计

DESIGN AND DEVELOPMENT OF REFRACTORY CERAMIC LINING FOR COMBUSTION CHAMBER OF UNCOOLED ROCKET MOTOR

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