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《Journal of Propulsion Technology》 2004-04
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Structural design analysis for platelet transpiration cooling section at throat of thrust chamber

YANG Wei-hua, CHENG Hui-er, WANG Ping-yang, WU LI-jun(Inst.of Thermophysics and Energy ,Shanghai Jiaotong Univ., Shanghai, 200030,China)  
According to the thermal analysis results of the platelet cell and the inherent characteristics of platelet transpiration cooling thrust chamber, the design principle and computational method of the advanced cooling project of rocket engine were brought forward. By the design to change the regeneration cooling into the transpiration cooling at the throat section of a 50kN liquid rocket engine thrust chamber, the design method of the platelet transpiration cooling section and the calculation results of main geometrical dimension were all analyzed. The temperature, thermal flux and weight between the complete regeneration cooling thrust chamber and transpiration cooling thrust chamber were all compared. The content can be helpful for the design of the advanced platelet transpiration cooling thrust chamber.
【CateGory Index】: V434.24
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1 YANG Wei hua, CHENG Hui er(School of Power and Energy Engineering , Shanghai Jiaotong Univ , Shanghai 200030, China);Experiment study for platelet slab flow channel control performance of platelet transpiration cooled thrust chamber[J];Journal of Propulsion Technology;2002-04
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