DocumentCode
2620367
Title
Development of a plasma armature railgun with two distributed power supplies
Author
Yamori, Akira ; Ono, Yukari ; Sasaki, Susumu
Author_Institution
Inst. of Space & Astronaut. Sci., Sagamihara, Japan
fYear
2005
fDate
25-28 May 2005
Firstpage
149
Lastpage
154
Abstract
We have been developing a plasma armature railgun with two distributed power supplies as the first step to produce a railgun with multiple distributed power supplies, which is considered as a promising tool for hypervelocities. The railgun has almost the same system and operational principle as those of the two-stage plasma armature railgun, which had been developed in our laboratory, except that the two power supplies are distributed along segmented rails or continuous rails. To date, we have performed 11 shots to study the railgun. For the operation of the railgun with two distributed power supplies, to control the generation of a compact plasma armature in the 2nd railgun bore is the most important. In 8 shots the compact structure of the plasma armature was not generated due to a large amount of leakage of the plasma armature around the joint between the two railguns. However in the remaining 3 shots, the deformation of the railgun bore around the railgun joint, which is considered to be the main reason for the leakage of the plasma armature, was able to be suppressed. As a result, the compact structure of the plasma armature in the 2nd railgun bore was generated. Based on the experimental results, we are now planning to perform the next-step experiment with a higher power supply energy.
Keywords
power supplies to apparatus; railguns; continuous rails; distributed generation control; hypervelocity; multiple distributed power supply; plasma armature leakage; plasma armature railgun; railgun bore; segmented rails; Acceleration; Boring; Cities and towns; Laboratories; Nuclear and plasma sciences; Plasma accelerators; Power supplies; Projectiles; Railguns; Rails;
fLanguage
English
Publisher
ieee
Conference_Titel
Electromagnetic Launch Technology, 2004. 2004 12th Symposium on
Print_ISBN
0-7803-8290-0
Type
conf
DOI
10.1109/ELT.2004.1398064
Filename
1398064
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