3.1 噪声的评价量 3.2 环境噪声的评价标准与法规

9.1 消声器性能评价 9.2 消声器的分类和消声机理 9.3 消声设计 9.4 消声设计工程实例

2.1 声音的产生和传播 2.2 声波的描述 2.3 声波的传播特性 2.4 声源的辐射特性

5.1 概述 5.2 环境噪声影响评价工作内容与程序 5.3 环境噪声预测

8.1 概述 8.2 隔声结构 8.3 隔声装置 8.4 隔声设计

5.1 噪声控制的基本原理与原则 5.2 城市环境噪声控制

4.1 测量仪器 4.2 声强及声功率测量 4.3 环境噪声监测方法

An ICBM with a range of 6500 miles has a stagnation temperature of 12,000 ºF, 2000 ºF hotter than the surface of the sun Calculations showed that the optimum design for structural strength, resistance to heating, and free flight stability was a long, needle nosed reentry body

Outline Purpose of thermal control systems Review of heat transfer fundamentals Space system thermal analysis Equations Models Analysis programs

Overview Ground Systems Support the space segment Command and Control Monitor spacecraft health Track Calculate spacecraft attitude