Librería: liu xing, Nanjing, JS, China
paperback. Condición: 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. Nº de ref. del artículo: CQ061676
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