EXPERIMENTAL INVESTIGATION OF THE TWO-STAGE PLASMA THRUSTER ATTILA

机译：两阶段等离子束流挡板的实验研究

获取原文

获取原文并翻译 | 示例

页面导航

摘要
著录项
相似文献
相关主题

摘要

Power characteristics of the inductive stage of the DC-HF hybrid thruster ATTILA are measured and interpreted using two di_erent induction coils (2.5 and 4.5 turns) under variation of ambient pressure. Test gases used are Nitrogen and Oxygen. At the present operation frequencies, generator power is coupled into the plasma with slightly higher e_ciency for Nitrogen than for Oxygen. E_ciencies determined for the inductive plasma generator are 44% and 43% in total. A rough ow characterization shows that ATTILA is a generator concept which, at the present stage of development, may reach 11.6N of thrust.

机译：在环境压力变化的情况下，使用两个不同的感应线圈（2.5和4.5匝）测量和解释DC-HF混合动力推进器ATTILA感应级的功率特性。所用的测试气体是氮气和氧气。在当前的工作频率下，发生器的功率耦合到等离子体中的氮效率比氧气高。确定的感应等离子体发生器的效率分别为44％和43％。粗略的流量表征表明，ATTILA是一种发电机概念，在目前的开发阶段，其推力可达到11.6N。

著录项

来源
《4th International spacecraft propulsion conference》|2004年|p.1-6|共6页
会议地点 Sardinia(IT)
作者
Hannah Boehrk; Joerg Weber; Stefan Laure; Georg Herdrich; Monika Auweter-Kurtz;
展开▼
作者单位

Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany;

Institut fur Raumfahrtsysteme (IRS), University of Stuttgart, Germany;

Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany;

Dr. Laure Plasmatechnologie GmbH, Stuttgart, Germany;

Institut fur Raumfahrtsysteme (IRS), University of Stuttgart, Germany;

Institut fur Raumfahrtsysteme (IRS), University of Stuttgart, Germany;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类推进系统（发动机、推进器）;
关键词
Hybrid plasma generator,DC-HF; power characteristic; coupling efficiency;

机译：混合等离子体发生器，DC-HF；功率特性耦合效率;

相似文献

外文文献
中文文献
专利

1. Experimental investigation on the plasma morphology of ablative pulsed plasma thruster with tongue-shaped and flared electrodes [J] . Wu Jianjun, Zhang Yu, Ou Yang, Plasma Science & Technology . 2020,第9期

机译：舌形和喇叭形电极烧蚀等离子推进器血浆形态的实验研究
2. Experimental investigation on the evolution of plasma properties in the discharge channel of a pulsed plasma thruster [J] . Plasma Science & Technology . 2020,第6期

机译：脉冲等离子体推进器排出通道中等离子体性能演化的实验研究
3. Experimental investigation on the plasma morphology of ablative pulsed plasma thruster with tongue-shaped and flared electrodes [J] . Jianjun WU, Yu ZHANG, Yang OU, 等离子体科学和技术（英文版） . 2020,第009期

机译：舌形和扩口电极烧蚀脉冲等离子体推进器等离子体形态的实验研究
4. EXPERIMENTAL INVESTIGATION OF THE TWO-STAGE PLASMA THRUSTER ATTILA [C] . Hannah Boehrk, Joerg Weber, Stefan Laure, International spacecraft propulsion conference . 2004

机译：两阶段等离子体推进器阿提列的实验研究
5. Experimental investigations of plasma parameters and species-dependent ion energy distribution in the plasma exhaust plume of a Hall thruster. [D] . Kim, Sang-Wook. 1999

机译：霍尔推力器等离子体排气羽中等离子体参数和物种相关离子能量分布的实验研究。
6. Experimental Investigation of Additive Manufacturing Using a Hot-Wire Plasma Welding Process on Titanium Parts [O] . Pattarawadee Poolperm, Wasawat Nakkiew, Nirut Naksuk 2021

机译：使用热线等离子体焊接工艺对钛件焊接工艺的实验研究
7. Experimental Investigation of High Frequency Plasma Oscillations within Hall Thrusters [O] . 2014

机译：霍尔推进器内高频等离子体振荡的实验研究
8. Experimental and Computational Investigation of a RF Plasma Micro- Thruster (Preprint); Technical paper [R] . Olliges, J. D., Ketsdever, A. D., Stein, W. B., 2008

机译：射频等离子体微推进器的实验和计算研究（预印本）;技术论文

EXPERIMENTAL INVESTIGATION OF THE TWO-STAGE PLASMA THRUSTER ATTILA

摘要

著录项

相似文献

相关主题

期刊订阅