Analysis of fusion propulsion system for Earth-to-Mars mission
文献类型：期刊论文
| 作者 | Song, Jun1,2; Chen, Zhibin1 ; Zeng, Qiusun1; Bai, Yunqing1; Wang, Fang1; Wu, Yican1
|
| 刊名 | FUSION ENGINEERING AND DESIGN
 |
| 出版日期 | 2021-03-01 |
| 卷号 | 164 |
| 关键词 | Fusion propulsion system Requirement analysis Earth-to-Mars mission |
| ISSN号 | 0920-3796 |
| DOI | 10.1016/j.fusengdes.2021.112230 |
| 通讯作者 | Chen, Zhibin(zhibin.chen@inest.cas.cn) |
| 英文摘要 | The high-performance space propulsion system is required for deep space exploration, such as Mars and Jupiter missions. The fusion propulsion system has an extraordinary performance of ultra-high specific impulse, high specific power, and moderate thrust, which can reflect its advantages in future deep space exploration missions. In this study, analysis has been conducted to investigate the technical requirements of the fusion propulsion system for the Earth-to-Mars mission. An analytical model based on Williams's assumption was adopted and solved by using the MATLAB code. Critical parameters such as specific impulse, specific power, mission time, and payload ratio for Mars rendezvous missions were analyzed. The qualitative and quantitative analysis results show that in order to reach Mars within one month with a payload ratio higher than 10 %, the specific power ranging from 5 to 15 kW/kg and the specific impulse of 10000 s is required. These parameters will take entirely inherent advantage of the fusion propulsion system. Moreover, the fusion propulsion system can operate under the optimal condition, including a wide range of the specific power (1-100 kW/kg) and the specific impulse (10000-200000 s). Based on a comprehensive analysis of the space mission performance, it is possible to provide a significant reference for the development of the fusion space propulsion system. |
| 资助项目 | Anhui Provincial Natural Science Foundation[1908085MA17] ; IAEA Coordinate Research Project[F13018] |
| WOS研究方向 | Nuclear Science & Technology |
| 语种 | 英语 |
| WOS记录号 | WOS:000632661700004 |
| 出版者 | ELSEVIER SCIENCE SA |
| 资助机构 | Anhui Provincial Natural Science Foundation ; IAEA Coordinate Research Project |
| 源URL | [http://ir.hfcas.ac.cn:8080/handle/334002/121397]  |
| 专题 | 中国科学院合肥物质科学研究院 |
| 通讯作者 | Chen, Zhibin |
| 作者单位 | 1.Chinese Acad Sci, Inst Nucl Energy Safety Technol, Key Lab Neutron & Radiat Safety, HFIPS, Hefei 230031, Anhui, Peoples R China 2.Univ Sci & Technol China, Hefei 230026, Anhui, Peoples R China |
| 推荐引用方式 GB/T 7714 | Song, Jun,Chen, Zhibin,Zeng, Qiusun,et al. Analysis of fusion propulsion system for Earth-to-Mars mission[J]. FUSION ENGINEERING AND DESIGN,2021,164. |
| APA | Song, Jun,Chen, Zhibin,Zeng, Qiusun,Bai, Yunqing,Wang, Fang,&Wu, Yican.(2021).Analysis of fusion propulsion system for Earth-to-Mars mission.FUSION ENGINEERING AND DESIGN,164. |
| MLA | Song, Jun,et al."Analysis of fusion propulsion system for Earth-to-Mars mission".FUSION ENGINEERING AND DESIGN 164(2021). |
入库方式： OAI收割
来源：合肥物质科学研究院
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