| 小卫星的推进系统 |
| |
| 引用本文： | 潘科炎.小卫星的推进系统[J].航天控制,1996(2). |
| |
| 作者姓名： | 潘科炎 |
| |
| 作者单位： | 北京控制工程研究所 |
| |
| 摘 要： | 小卫星推进系统可以完成多种功能：变轨、轨道保持、姿态控制、重新定位以及离轨等。先进化学推进系统和低功耗电推进系统是现代小卫星的理想选择。近期可供小卫星应用的推进系统包括高压Ｉｒ／Ｒｅ双组元推力器、电弧推力器、霍尔推力器、脉冲等离子体推力器。业已证明，这些推进系统可以在目前计划中的许多小卫星上发挥其用武之地。本文综述了这一技术领域的最新进展。
|
| 关 键 词： | 小卫星，推进系统，应用 |
Propulsion Systems for Small Satellites |
| |
| Pan Keyan.Propulsion Systems for Small Satellites[J].Aerospace Control,1996(2). |
| |
| Authors: | Pan Keyan |
| |
| Institution: | Beijing Institute of Control Engineering.100080 |
| |
| Abstract: | Propulsion functions on small satellites includeorbit raising,orbit maintenance,attitude control,repositioning and deorbit.Advanced chemical and low power electric propulsion systems offer attractive options for near-term small satellite pro pulsion systems,inchuding high pressure Ir/Re bipropellant rochet engines, arejets,Hall thrusters,and pulsed plasma thrusters,All of which have been shown to operate in manners consitent with planned small satellites.The newest development is serveyed in this paper. |
| |
| Keywords: | Small satellite Propulsion system Application |
| 本文献已被 CNKI 等数据库收录！ |
