arcjet

arcjet

1. Radiation inside a Low Power Argon Arcjet Thruster

低功率氩电弧喷射推力器中的辐射

2. Experimental investigation of low power arcjet thrusters

低功率电弧喷射推力器实验研究

3. Arcjet impulse

发动机比冲

4. Temperature measurement of arcjet plume with emission spectrum

发射光谱测量电弧加热发动机羽流温度

5. In vacuum environment, the performances of the arcjet were tested under several conditions with argon as the propellent.

在真空环境下,用氩作推进剂,得到了不同工况下发动机的性能参数.

6. Some working phenomena of the arcjet are observed and discussed.

对所观察到的一些工作现象进行了讨论。

7. WORK PROCESS AND PERFORMANCE EXPERIMENT OF A LOW POWER NITROGEN ARCJET

推进剂电弧推力器工作过程和性能实验

8. 1.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。

9. A Langmuir probe diagnostic system for Arcjet plume is established first in China, in which Langmuir probe is employed to obtain the electron temperature of the Arcjet plume with argon propellant.

本文建立了一套静电探针诊断系统,在国内首次对以氩气为推进剂的电弧加热发动机羽流电子温度进行了测量。

10. Hydrogen distribution in CVD diamond films prepared by DC arcjet operating at gas recycling mode[J]; Journal of University of Science and Technology Beijing; 2002年06期; 43-45

汤海滨,姬罗栓,刘宇,戴梧叶;小功率电弧等离子体发动机实验数据采集系统[J];北京航空航天大学学报;2001年05期;125-128

11. Influence of Environmental Pressure on Arcjet Thruster Performance

环境压强对电弧喷射推力器性能的影响

12. Arcjet thrusters

电弧加热发动机

13. Keywords arcjet;water;stability;capillary bundle;spectral line intensity method;

电弧加热发动机;水;稳定性;毛细管束;谱线强度法;

14. Keywords arcjet;water;plume;spectral diagnostic;Langmuir probe;

电弧加热发动机;水;羽流;光谱诊断;朗谬尔探针;

15. Keywords Arcjet;Plasma;Plume;Diagnostics;Numerical simulation;

电弧加热发动机;等离子;羽流;诊断;数值模拟;

16. Arcjet, one type of electric propulsion, is high at specific impulse and ratio of thrust, and good in capability of propellant.

电弧加热发动机就是电推进的一种,它具有较高的比冲和推力/功率比以及良好的推进剂普适性,已成为国际研究和应用的重点。

17. Effects of Arcjet Thruster Structure Parameters on Performance

电弧加热发动机结构参数对性能的影响

18. Arcjet Plume Plasma Measurements Using Electrostatic Probe

电弧加热发动机羽流电子温度的探针诊断

19. Arcjet thruster

电弧加热推力器

20. electrical arcjet engines

电弧喷射推力器

21. Chemical non-equilibrium simulation on arcjet thrusters

电弧喷射推力器化学非平衡数值模拟

22. Modeling of electromagnetic field within arcjet thruster

电弧喷射推力器电磁场模拟

23. arcjet engine

电弧喷气式发动机

24. For the same conditions, the thermal efficiency of the original arcjet was from 21% to 32%, where the thermal efficiency of the new arcjet was from 32% to 52%.

相同工况下,原发动机效率为21%~23%,新发动机效率为32%~53%。

25. has multifarious effects on arcjet thruster operation, and both specific impulse and thrust efficiency can be improved by increasing it befittingly under steady arc.

研究表明，集气腔总压对推力器工作过程具有多方面的影响，在保证电弧稳定的情况下，适当提高集气腔总压可同时提高比冲和推进效率。

26. mag - netohydrodynamic arcjet

磁流体动力电弧火箭发动机

27. 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。

28. Numerical study on hydrazine arcjet thruster working exchangeability

肼电弧喷射推力器工作方式可替换性数值研究

29. An annular cavity placed around the anode of arcjet was designed to form a regenerative cooling channel on the base of an arc jet.

该文在原有电弧加热发动机基础上进行改进，设计了覆盖发动机阳极的环形空腔，形成再生冷却通道。

30. Effect of plenum chamber total pressure on arcjet thruster operation

集气腔总压对电弧喷射推力器工作过程的影响

31. Investigation on computation method of LTE model parameter for high temperature gases and its application in the state diagnosis of non-equilibrium arcjet

高温气体LTE模型参数计算方法及其在非平衡电弧射流状态诊断中的应用研究