(9) Solid propellant rocket engines, having a total impulse capacity of 1100 kN·s or greater;

    （十）能使射程为300千米的弹道导弹的精度达到10千米或以下圆公算偏差的制导装置

(10) Guidance sets capable of achieving system accuracy of 10 km or less (CEP) for ballistic missiles with a range of 300 km;

    （十一）推力矢量控制系统

(11) Thrust vector control sub-systems;

    （十二）弹头保险、解保、引信和起爆装置

(12) Warhead safing, arming, fuzing, and firing mechanisms;

    （十三）为上述第（一）至第（十二）项专门设计的生产设施与设备

(13) Production facilities and equipments designed for Subitems (1) to (12).

    三、运载火箭的级间机构及为其专门设计的生产设备

3. Interstage mechanisms for space launch vehicles and the specially designed production equipment therefor.

    四、火箭发动机的壳体及为其专门设计的生产设备

4. Rocket motor cases and the specially designed production equipment therefor.

    五、专门设计或改进用于第一部分第一项中各系统的液压、机械、光电或机电控制系统

5. Hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems specially designed or modified for the systems in Item 1 of Part I.

    六、专门设计或改进用于第一部分第一项中各系统的姿态控制设备

6. Attitude control equipment specially designed or modified for the systems in Item 1 of Part I.

    七、为了优化无人驾驶航空飞行器在整个飞行过程中的空气动力特性而使机身、推进系统和升力控制面一体化的设计技术

7. Design technology for integration of air vehicle fuselage, propulsion system and lifting control surfaces to optimize aerodynamic performance throughout the flight regime of an unmanned air vehicle.

    八、为了优化导弹或火箭弹道而使制导、控制和推进数据一体化成为一个飞行管理系统的设计技术

8. Design technology for integration of the guidance, flight control, and propulsion data into a flight management system for optimization of trajectory of ballistic missiles or space launch vehicles.

    九、能用于第一项中各系统的无源电子干扰设备

9. Passive interferometer equipment usable in the systems in Item 1.

    十、为第一项的装卸、控制、待发射和发射而设计或改进的仪器和装置

10. Apparatus and devices designed or modified for the handling, control, activation and launching of the systems in Item 1.

    十一、为第一项的运输、装卸、控制、待发射和发射而设计或改进的车辆

11. Vehicles designed or modified for the transport, handling, control, activation and launching of the systems in Item 1.

    十二、静态或工作状态精度为1毫伽或更好、达到稳态记录时间至多为2分钟的机载或舰载重力仪、重力梯度仪及为其专门设计的部件

12. Gravity meters, gravity gradiometers, and specially designed components therefor, for airborne or marine use, and having a static or operational accuracy of one milligal or better, with a time to steady-state registration of two minutes or less;

    十三、精密跟踪系统

13. Precision tracking systems:

    （一）安装在火箭系统或无人驾驶航空飞行器上的采用转发器的跟踪系统，它连同地面或空中的参考基准或导航卫星系统可提供飞行中位置和速度的实时测量数据

(1) Tracking systems which use a translator installed on the rocket system or unmanned air vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity;

    （二）用来事后处理记录数据，从而能够确定飞行器在整个飞行轨迹中的位置的软件

(2) Software which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path.

    十四、降低雷达波反射特性的结构件

14. Structure specially designed for reduced radar reflectivity.

    十五、用来降低雷达波反射特性的结构材料

15. Structural material specially designed for reduced radar reflectivity.

    十六、用来降低雷达波反射特性的涂料

16. Coatings specially designed for reduced radar reflectivity.

    十七、专门设计用来降低光学反射或辐射的涂料

17. Coatings specially designed for reduced optical refle

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