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Method for On-Orbit Thrust Estimation for Microthrusters Based on Nanosatellites
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-27 , DOI: 10.1061/(asce)as.1943-5525.0001370 Qinglin Yang 1 , Weijing Zhou 2 , Jifei Ye 3 , Hao Chang 4
Journal of Aerospace Engineering ( IF 1.5 ) Pub Date : 2021-11-27 , DOI: 10.1061/(asce)as.1943-5525.0001370 Qinglin Yang 1 , Weijing Zhou 2 , Jifei Ye 3 , Hao Chang 4
Affiliation
The development of nanosatellites is inseparable from micropropulsion systems, and
a micropropulsion system cannot be separated from the evaluation of its micropropulsion
performance. Although the ground measurement system is relatively mature, it ...
中文翻译:
基于纳米卫星的微型推进器在轨推力估计方法
纳米卫星的发展离不开微推进系统,而一个微推进系统也离不开对其微推进性能的评价。虽然地面测量系统相对成熟,但它...
更新日期:2021-11-27
中文翻译:
基于纳米卫星的微型推进器在轨推力估计方法
纳米卫星的发展离不开微推进系统,而一个微推进系统也离不开对其微推进性能的评价。虽然地面测量系统相对成熟,但它...