| 1. | Techniques of measurement for flow properties in arcjet
电弧加热发动机参数的测量技术 |
| 2. | So it has important significance to investigate the arcjet system
因此,开展对电弧加热发动机的研究具有十分重要的意义。 |
| 3. | Basic specifications for electroheat installations part 2 : arc electroheat installations
电热装置基本技术条件第2部分：电弧加热装置 |
| 4. | A low power arcjet with high performance has been designed and constructed in this dissertation
本文设计、建造一套性能先进的低功率电弧加热发动机。 |
| 5. | Arcjet which used water as propellant has special advantage in deep space exploration and manned spacecraft
以水作为推进剂的电弧加热发动机,在深空探测和载人航天中具有独特的优势。 |
| 6. | It is necessary to do study on it as a request of the development of small satellites and future aerospace tasks
鉴于我国当前小卫星的蓬勃发展以及未来航天任务的需要,研制低功率电弧加热发动机是很有必要的。 |
| 7. | Advanced arcjet system will be one of the favorite choices with the development of space technology and the demand of aerospace task
随着空间技术的发展和未来航天任务的需求,先进的电弧加热发动机将是理想的选择。 |
| 8. | A kind of low power arcjet structure is designed , produced and combined in this thesis . an experimental system was also built up
本文设计了一种低功率电弧加热发动机的原理结构,完成了发动机的加工、组装和试验系统的组建。 |
| 9. | The two - dimensional axisymmetric subsonic - transonic - supersonic flow in an experimental arcjet thruster is simulated numerically using flux vector splitting method
摘要对一实验电弧加热式发动机二维轴对称亚跨超音速流动进行了数值模拟，所采用的方法是矢通量分裂算法。 |
| 10. | The test equipment such as power supply system , ignition system , propellant supply system , arcjet thruster , thrust measuring device and vacuum system are introduced briefly
简要介绍了实验所使用的设备，如电源系统、点火系统、推进剂供给系统、电弧加热式发动机、推力测量装置和真空系统。 |
