基于离子电推进系统的航天器有效载荷能力分析
赖承祺,顾左,宋莹莹,王蒙,郭伟龙,吴辰宸
Analysis of Spacecraft Payload Capacity Based on Ion Propulsion System
LAI Cheng-qi
1,GU Zuo
1,SONG Ying-ying
1,WANG Meng
1,GUO Wei-long
1,Wu Chen-chen
1
推进技术
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2019, (10): 2183
-2189
.
DOI: 10.13675/j.cnki. tjjs. 180685
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