TY - JOUR
T1 - Research on electromagnetic propulsion system based on reusable space vehicle
AU - Hui, Fu
AU - Pei, Wang
AU - Ke, Zhang
AU - Mei Bo, Lv
AU - Zhi Lei, Ge
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
PY - 2018/6/27
Y1 - 2018/6/27
N2 - It is inefficient and uneconomical to complete space launch mission with the assistance of unusable rockets which is the typically used approach today, and finding a more economical way has been the pursuit of scholars all over the world. According to the purpose above, this paper proposed a new design to lift a payload to the desired orbit. In this design, the electromagnetic propulsion system (EMPS) is applied to replace the first rocket, leaving the usable rocket to take care of the rest job. Based on this design, the structure of the propulsion system is constructed and the electromagnetic properties are analyzed by finite element analysis tool Maxwell, then the mathematic model of EMPS is simulated and calculated. The result shows that EMPS is capable of accelerating the vehicle, which weighs hundreds of tons, up to one hundred meters per second. Therefore, it is foreseeable that EMPS has a certain potential in the future space launch mission.
AB - It is inefficient and uneconomical to complete space launch mission with the assistance of unusable rockets which is the typically used approach today, and finding a more economical way has been the pursuit of scholars all over the world. According to the purpose above, this paper proposed a new design to lift a payload to the desired orbit. In this design, the electromagnetic propulsion system (EMPS) is applied to replace the first rocket, leaving the usable rocket to take care of the rest job. Based on this design, the structure of the propulsion system is constructed and the electromagnetic properties are analyzed by finite element analysis tool Maxwell, then the mathematic model of EMPS is simulated and calculated. The result shows that EMPS is capable of accelerating the vehicle, which weighs hundreds of tons, up to one hundred meters per second. Therefore, it is foreseeable that EMPS has a certain potential in the future space launch mission.
UR - http://www.scopus.com/inward/record.url?scp=85049884398&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1039/1/012041
DO - 10.1088/1742-6596/1039/1/012041
M3 - 会议文章
AN - SCOPUS:85049884398
SN - 1742-6588
VL - 1039
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012041
T2 - 2018 8th International Conference on Applied Physics and Mathematics, ICAPM 2018
Y2 - 27 January 2018 through 29 January 2018
ER -