【新书推荐】【2019.10】化学火箭性能预测与内弹道设计

本书的目的是在研究生水平讨论化学火箭推进性能预测的方法。

The purpose of this book is to discuss, at the graduate level, the methods of performance prediction for chemical rocket propulsion.

到目前为止，还没有关于这种方法的教学介绍，本书以讲座为基础填补了这一空白。

A pedagogical presentation of such methods has been unavailable thus far and this text, based upon lectures, fills this gap.

第一部分包括计算推进剂燃烧组分的能量最小化和随后的火箭性能计算。

The first part contains the energy-minimization to calculate the propellant-combustion composition and the subsequent computation of rocket performance.

增量分析适用于高性能固体发动机，平衡压力分析适用于低性能固体发动机。

While incremental analysis is for high performance solid motors, equilibrium-pressure analysis is for low performance ones.

这两种方法都在书的第二部分：预测点火、尾流瞬变以及平衡运行中进行了详细阐述。

Both are detailed in the book’s second part for the prediction of ignition and tail-off transients, and equilibrium operation.

包括了采用增量分析的计算机程序。

Computer codes, adopting the incremental analysis along with erosive burning effect, are included.

鼓励在课堂上使用并演示这些材料。

The material is encouraged to be used and presented at lectures.

本书主要针对大学高年级本科生和研究生，以及火箭工业的工程师和科学家。

Senior undergraduate and graduate students in universities, as well as practicing engineers and scientists in rocket industries, form the readership.

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