@inproceedings{881058d9fa9045b2b4efb9657002bd2f,
title = "Feasibility analysis of electromagnetic assisted launch technology for two-stage orbiting launch vehicle",
abstract = "Based on the research and feasibility analysis of the launch vehicle's electromagnetic assisted technology, this paper takes the two-stage launch vehicle as the research object, and aims to improve the carrying capacity of the launch vehicle. The results show that the medium-sized rocket launches at an initial velocity of not less than 2.26km/s when the electromagnetic assisted launch, the two-stage orbital scheme is feasible; and the large-scale rocket can achieve two-level orbiting without adding the electromagnetic auxiliary launching link.",
keywords = "Electromagnetic propulsion, Feasibility analysis, Two-stage orbiting rocket",
author = "Jianhua Feng and Xin Zhang and Lili Liu and Rongjun Mu",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 6th International Conference on Information Science and Control Engineering, ICISCE 2019 ; Conference date: 20-12-2019 Through 22-12-2019",
year = "2019",
month = dec,
doi = "10.1109/ICISCE48695.2019.00213",
language = "英语",
series = "Proceedings - 2019 6th International Conference on Information Science and Control Engineering, ICISCE 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1058--1062",
editor = "Shaozi Li and Yun Cheng and Ying Dai and Jianwei Ma",
booktitle = "Proceedings - 2019 6th International Conference on Information Science and Control Engineering, ICISCE 2019",
address = "美国",
}