TY - GEN
T1 - Influence on launching velocity by the figure and material characteristic of projectiles
AU - Li, Xiaopeng
AU - Tian, Ku
AU - Zhou, Yuan
AU - Li, Yi
AU - Zhang, Chengming
PY - 2008
Y1 - 2008
N2 - A solid metal plate is often used as the projectile in reconnection electromagnetic launcher. Yet the performance is not optimum. In this paper, analysis is made about the laws of influence on magnetic field distribution of driving coils by using projectiles with different figures and materials. Further analysis is made about the influence on launching velocity of the above factors. A single-stage reconnection electromagnetic launcher is made. Experiments are carried out separately on latticed projectiles, hollow projectiles, aluminium projectiles, iron projectiles and copper projectiles. Some significant conclusions are drawn. Under the same condition, hollow projectiles achieve the highest velocity, while latticed projectiles have a weaker shielding effect upon magnetic field. The magnetic permeability and electric conductivity of material have a great influence upon launching velocity. Based on magnetic domain theory, qualitative analysis is made about the causation of magnetic hysteresis loss, classical eddy current loss and abnormal loss. As the loss under high-frequency alternating magnetic field increasing rapidly, ferromagnetic materials are not suitable here. The electric conductivity of projectiles, as well as the thickness and the density makes sense to launching velocity. As the frequency grows higher in pulsed magnetic field, the influence from thickness and electric conductivity of projectiles becomes weaker. Therefore, hollow projectiles made up of aluminium material which has a higher electric conductivity and a lower density will be the best choice.
AB - A solid metal plate is often used as the projectile in reconnection electromagnetic launcher. Yet the performance is not optimum. In this paper, analysis is made about the laws of influence on magnetic field distribution of driving coils by using projectiles with different figures and materials. Further analysis is made about the influence on launching velocity of the above factors. A single-stage reconnection electromagnetic launcher is made. Experiments are carried out separately on latticed projectiles, hollow projectiles, aluminium projectiles, iron projectiles and copper projectiles. Some significant conclusions are drawn. Under the same condition, hollow projectiles achieve the highest velocity, while latticed projectiles have a weaker shielding effect upon magnetic field. The magnetic permeability and electric conductivity of material have a great influence upon launching velocity. Based on magnetic domain theory, qualitative analysis is made about the causation of magnetic hysteresis loss, classical eddy current loss and abnormal loss. As the loss under high-frequency alternating magnetic field increasing rapidly, ferromagnetic materials are not suitable here. The electric conductivity of projectiles, as well as the thickness and the density makes sense to launching velocity. As the frequency grows higher in pulsed magnetic field, the influence from thickness and electric conductivity of projectiles becomes weaker. Therefore, hollow projectiles made up of aluminium material which has a higher electric conductivity and a lower density will be the best choice.
KW - Electromagnetic launcher
KW - Material characteristic
KW - Reconnection
UR - https://www.scopus.com/pages/publications/57849117453
U2 - 10.1109/ELT.2008.127
DO - 10.1109/ELT.2008.127
M3 - 会议稿件
AN - SCOPUS:57849117453
SN - 9781424418336
T3 - 2008 14th Symposium on Electromagnetic Launch Technology, EML, Proceedings
SP - 603
EP - 606
BT - 2008 14th Symposium on Electromagnetic Launch Technology, EML, Proceedings
T2 - 2008 14th Symposium on Electromagnetic Launch Technology, EML
Y2 - 10 June 2008 through 13 June 2008
ER -