| 1. | The saturn i launch vehicles consisted of two types or blocks .
“土星”发射飞行器包括两类或两个组合。 |
| 2. | The saturn family of launch vehicles falls into three types or groups .
“土星族”发射飞行器可以分成为三类或三组。 |
| 3. | It should be pointed out that some launch vehicles or missiles are usually unstable .
应该指出，某些发射飞行器或导弹总是不稳定的。 |
| 4. | "aerodynamics" defines the pressure fields and loads that exist on a launch vehicle due to the reaction of ambient flow .
“空气动力学”规定了由于绕流反作用在发射飞行器上存在的压力场和载荷。 |
| 5. | Located atop the s-ivb, which is the third stage of the saturn v, is the guidance and control equipment for the launch vehicle .
安装在“土星V”第三级S-IVB顶部的是发射飞行器的导航和控制设备。 |
| 6. | This monograph is focused primarily upon wind effects on large launch vehicles as represented by the family of saturn vehicles .
这个专著，主要集中研究大型发射飞行器上风的影响，以“土星族”飞行器为代表。 |
| 7. | The principal perturbing forces for launch vehicles, both on the launch pad and in flight, are the aerodynamic loads produced by winds .
发射飞行器在发射台上以及在飞行中的重要扰动力是由风产生的气动载荷。 |
| 8. | Located atop the s - ivb , which is the third stage of the saturn v , is the guidance and control equipment for the launch vehicle
安装在“土星v ”第三级s - ivb顶部的是发射飞行器的导航和控制设备。 |
| 9. | It was analyzed about the problems of space vehicle flight control , the development of space vehicles , the design aim and main characteristic of flight control systems of varied space vehicles , the main design requirement of flight control system of reusable space vehicles , the key technology which have to be resolved in flying control law design and flight control system design
摘要分析了空间飞行器飞行控制系统要解决的问题，空间飞行器的发展过程，各类空间飞行器飞行控制系统设计目的和主要特点，可重复使用的发射飞行器飞控系统的主要设计要求，在设计要求的确定，飞行控制律设计和飞行控制系统设计中要解决的关键技术。 |
