TY - GEN
T1 - Fundamental study on reconnection. Electromagnetic launch assist technology
AU - Li, Liyi
AU - Li, Xiaopeng
AU - Luo, Guangyao
AU - Zou, Jiyan
PY - 2003
Y1 - 2003
N2 - With the ever-increasing cost of getting to space and the need for safe, reliable, and inexpensive ways to space, many researchers are taking a look at technologies that will get us to space. One of these technologies is Electromagnetic Launch Assist (EMLA). This is the concept of providing the rocket with an initial velocity by using electrical power from ground sources to save fuel and cut down cost. In this paper, the shortages of chemical launch and the fundamental work process of reconnection electromagnetic launcher is described briefly, the fundamental performance of simple reconnection electromagnetic launcher and the effect law that the parameter of driving coil and planked projectile pose on their fundamental performance, and all of these will be a basis of the design for reconnection electromagnetic launcher. And then, based on the features of simple reconnection electromagnetic launcher, the simulation and research for simple system of reconnection Eh4LA are put forward. The result shows that, using this system, we could make the load of about 1 OOOOkg accelerate to the velocity of 180ds with 32 times the acceleration of gravity and then save cost of launch vehicle.
AB - With the ever-increasing cost of getting to space and the need for safe, reliable, and inexpensive ways to space, many researchers are taking a look at technologies that will get us to space. One of these technologies is Electromagnetic Launch Assist (EMLA). This is the concept of providing the rocket with an initial velocity by using electrical power from ground sources to save fuel and cut down cost. In this paper, the shortages of chemical launch and the fundamental work process of reconnection electromagnetic launcher is described briefly, the fundamental performance of simple reconnection electromagnetic launcher and the effect law that the parameter of driving coil and planked projectile pose on their fundamental performance, and all of these will be a basis of the design for reconnection electromagnetic launcher. And then, based on the features of simple reconnection electromagnetic launcher, the simulation and research for simple system of reconnection Eh4LA are put forward. The result shows that, using this system, we could make the load of about 1 OOOOkg accelerate to the velocity of 180ds with 32 times the acceleration of gravity and then save cost of launch vehicle.
UR - https://www.scopus.com/pages/publications/84879333448
U2 - 10.1109/AERO.2003.1235197
DO - 10.1109/AERO.2003.1235197
M3 - 会议稿件
AN - SCOPUS:84879333448
SN - 078037651X
SN - 9780780376519
T3 - IEEE Aerospace Conference Proceedings
SP - 2717
EP - 2723
BT - 2003 IEEE Aerospace Conference, Proceedings
T2 - 2003 IEEE Aerospace Conference
Y2 - 8 March 2003 through 15 March 2003
ER -