深空探测聚变推进装置技术路线与研究现状综述  

Review of Technical Strategies and Research Status for Deep Space Fusion Propulsion Explorer

作　　者：李凤臣 汤颖杰 赵俊龙 李小斌 张红娜 周成[2] 李永[2] 郑金星[3] LI Feng-chen;TANG Ying-jie;ZHAO Jun-long;LI Xiao-bin;ZHANG Hong-na;ZHOU Cheng;LI Yong;ZHENG Jin-xing(Key Laboratory of Efficient Utilization of Low and Medium Grade Energy,Ministry of Education,School of Mechanical Engineering,Tianjin University,Tianjin 300350,China;Beijing Institute of Control Engineering,Beijing 100094,China;Institute of Plasma Physics,Chinese Academy of Sciences,Hefei 230031,China)

机构地区：[1]天津大学机械工程学院中低温热能高效利用教育部重点实验室,天津300350 [2]北京控制工程研究所,北京100094 [3]中国科学院等离子体物理研究所,安徽合肥230031

出　　处：《推进技术》2023年第6期12-27,共16页Journal of Propulsion Technology

摘　　要：聚变推进技术凭借其能量密度大和高比冲等显著优势,在深空探测研究中受到广泛关注。本文介绍了三种前沿聚变推进装置(反场构型感应驱动金属衬层压缩聚变推进探测器、梯度场内爆衬层聚变推进探测器和普林斯顿反场构型直接聚变驱动探测器)的研究进展,从聚变堆设计原理、深空探测任务参数与实验进展等角度,对三种技术路线进行了分析和总结。Fusion propulsion system has attracted wide attention in deep space exploration because of its re⁃markable advantages,such as high energy density and high specific impulse.The research progress of three fron⁃tier fusion drive rocket(inductively-driven metal shell compression fusion propulsion spacecraft,gradient field implosion liner fusion propulsion spacecraft and fusion direct drive powered spacecraft)is introduced.The three technical routes are analyzed and summarized from the view of fusion reactor principle,deep space exploration mission parameters and experimental progress.

关 键 词：聚变推进火箭 深空探测 直接聚变驱动 反场构型 磁约束聚变推进探测器 磁惯性约束聚变推进探测器 综述 

分 类 号：V439.5[航空宇航科学与技术—航空宇航推进理论与工程]