Language:Chinese.Pub Date: 2014-09-01 Pages: 317 Publisher: National Defense Industry Press Wang Zhijun. Chang Xin Long. Tin dry. Zhang Xiaojun compiled the liquid rocket engine thrust chamber design (fine). The book consists of 11 chapters. Introduction Chapter 1 introduces the basic principle of the thrust chamber. Chapter 2 of the liquid propellant thrust chamber used to make a brief introduction. because the propellant in some of the performance parameters of the original data to calculate the thermodynamic parameters thrust chamber. Chapter 3 thermodynamic parameters calculated on the basis of the analysis of the thermodynamic process introduces the calculation method of the thrust chamber performance parameters and geometry. The first chapter 4.5.8.10 structural design principle and method of each part of the thrust chamber. the design makes specific introduction. Chap...
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Seller: liu xing, Nanjing, JS, China
paperback. Condition: New. Language:Chinese.Pub Date: 2014-09-01 Pages: 317 Publisher: National Defense Industry Press Wang Zhijun. Chang Xin Long. Tin dry. Zhang Xiaojun compiled the liquid rocket engine thrust chamber design (fine). The book consists of 11 chapters. Introduction Chapter 1 introduces the basic principle of the thrust chamber. Chapter 2 of the liquid propellant thrust chamber used to make a brief introduction. because the propellant in some of the performance parameters of the original data to calculat. Seller Inventory # CQ061676
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