JPH043896A - Method and device for forming plasma armature of rail gun type electromagnetic accelerator - Google Patents
Method and device for forming plasma armature of rail gun type electromagnetic acceleratorInfo
- Publication number
- JPH043896A JPH043896A JP2102401A JP10240190A JPH043896A JP H043896 A JPH043896 A JP H043896A JP 2102401 A JP2102401 A JP 2102401A JP 10240190 A JP10240190 A JP 10240190A JP H043896 A JPH043896 A JP H043896A
- Authority
- JP
- Japan
- Prior art keywords
- plasma
- rail
- type electromagnetic
- current
- hole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Plasma Technology (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
この発明は、レールガン型電磁加速装置に関するもので
ある。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a rail gun type electromagnetic accelerator.
電磁力を用いて巨視的な物体を高速に加速するレールガ
ン型電磁加速装置(以下レールガンと呼ぶ)は、火薬の
燃焼ガスや高圧ガスの膨張力を用いる方式では達成が困
難な、秒速10km/s以上の飛翔体速度を得ることが
可能とされ、近年注目されている。A railgun-type electromagnetic accelerator (hereinafter referred to as a railgun) uses electromagnetic force to accelerate macroscopic objects at high speeds, which is difficult to achieve with methods that use the combustion gas of gunpowder or the expansion force of high-pressure gas. It has been attracting attention in recent years as it is possible to obtain projectile speeds higher than the above.
レールガンの電機子のための材料としては、固体金属と
プラズマの2種類が用いられているが、特にプラズマ電
機子を用いる方式は、重量が数グラムの小型飛翔体を超
高速に加速する場合に主として採用され、例えば、物質
同志の衝突により1000万気圧以上の衝撃超高圧力を
発生させるための加速装置として、また宇宙空間におけ
る陽石衝突問題のシミュレーション装置として、さらに
は核融合炉への固体水素燃料ペレット打ち込み装置等へ
の利用が期待され、実用化へ向けての開発が盛んに行な
われている。Two types of materials are used for the armature of a railgun: solid metal and plasma, but the method using a plasma armature is particularly useful when accelerating a small flying object weighing a few grams to ultra-high speed. It is mainly used as an accelerator to generate shock ultra-high pressure of more than 10 million atmospheres through the collision of materials, as a simulation device for the problem of rock collisions in outer space, and as a solid material for nuclear fusion reactors. It is expected to be used in hydrogen fuel pellet implantation equipment, etc., and development toward practical use is actively underway.
レールガンの研究開発とその利用技術に関しては、IE
EE Transactions on Magnet
ics、 vol、Mag20、No、2(1984)
、 vol、 Wag−22,No、(1986)、及
び、vol、25. No1(1989)の諸論文に紹
介されている。Regarding research and development of railguns and their utilization technology, please refer to IE
EE Transactions on Magnet
ics, vol, Mag20, No. 2 (1984)
, vol. Wag-22, No. (1986) and vol. 25. No. 1 (1989).
プラズマ電機子を用いるレールガンの加速原理および構
造を第3図fa)、(blに示した。2本のレール状電
極1間の加速孔2内に絶縁物の飛翔体3を設置し、その
背後にプラズマ電機子形成用の金属板あるいは金属箔4
を設置して、2本のレール電極間が電気的に接触するよ
うにする。この状態でキャパシターバンク等の生霊B
5を2本のレールに接続しスイッチ6を閉じて電源電圧
を付加すると、第3図(blのように金属板あるいは金
属箔は大電流によりプラズマ化する。このプラズマ7は
し・−ル間の電流を保ちつつ、電磁誘導の法則による電
磁力を受けて飛翔体に力を及ぼし加速する。このプラズ
マ7は、飛翔体と共に移動して常に飛翔体背後に位置す
る電機子としての役割を果たし、電流の2乗に比例する
力で飛翔体を加速し続ける。The acceleration principle and structure of a railgun using a plasma armature are shown in Figure 3fa) and (bl).An insulating flying object 3 is installed in an acceleration hole 2 between two rail-shaped electrodes 1, and a A metal plate or metal foil for forming a plasma armature 4
is installed to make electrical contact between the two rail electrodes. In this state, the ghost B of the capacitor bank etc.
When 5 is connected to two rails, switch 6 is closed, and power supply voltage is applied, the metal plate or metal foil becomes plasma due to the large current as shown in Figure 3 (bl). While maintaining a current of , continues to accelerate the projectile with a force proportional to the square of the current.
レールガンによる飛翔体加速においては、加速初期の飛
翔体速度が遅い時点で、レール電極表面に著しい損傷が
生じる。これは加速初期においてはプラズマ電機子の移
動速度が遅く、レール電極表面の狭い領域に大電流が集
中してしまうためである。レール電極表面の損傷は加速
孔の断面形状を機械的に変形させるのみならず、プラズ
マ電機子の質量増加をもたらし加速効率を低下させる。When accelerating a projectile using a rail gun, significant damage occurs to the surface of the rail electrode when the speed of the projectile is slow at the beginning of acceleration. This is because the moving speed of the plasma armature is slow in the early stages of acceleration, and a large current is concentrated in a narrow region on the surface of the rail electrode. Damage to the surface of the rail electrode not only mechanically deforms the cross-sectional shape of the acceleration hole, but also increases the mass of the plasma armature and reduces acceleration efficiency.
そのため、N if!加速する飛翔体をあらかじめ他の
方法で初期加速し、電磁加速初期のプラズマ電機子の移
動速度をできるだけ増して、レール表面の損傷を軽減さ
せる方式が一般化している。この場合、初期加速されて
レールガン内に入射した飛翔体の背後にプラズマ電機子
を形成することが必要であり、その方法として、
(1)絶縁物の飛翔体の背面にあらかじめ金属箔等のプ
ラズマ形成材料を接着しておき、金属箔が飛翔体と共に
レールガンに入射してレール電極間を短絡した時点で、
レール電極間に主inの電圧を荷して金属箔をプラズマ
化する方法(例: S、USUB^KJONDO,S、
5AWAOKA、IEEE Transacti
ons on Magnetics、 vol、M
ag−20+ No、2+ p260(1984))と
、(2)レールガン加速孔内の絶縁体表面上に付加的な
一対の点電極を露出させ、その位置を飛翔体が通過した
後に、高圧電源を用いて点電極間にスパークを起こさせ
、それと同期してレール電極間に主電源の電圧を荷して
、その場所でのレール電極間の絶縁破壊を誘起しアーク
放電を開始させる方法(例: R,S、HAWKE、e
t、al、IEEE Transactions on
Magnetics、vol、25.p219(198
9))がある。Therefore, N if! It has become common practice to reduce damage to the rail surface by initially accelerating the accelerating projectile using another method and increasing the moving speed of the plasma armature as much as possible at the initial stage of electromagnetic acceleration. In this case, it is necessary to form a plasma armature behind the projectile that is initially accelerated and enters the rail gun.The methods for this are: The forming material is glued together, and when the metal foil enters the rail gun together with the flying object and shorts between the rail electrodes,
A method of turning metal foil into plasma by applying a main voltage between rail electrodes (e.g. S, USUB^KJONDO, S,
5AWAOKA, IEEE Transacti
ons on Magnetics, vol, M
ag-20+ No, 2+ p260 (1984)) and (2) an additional pair of point electrodes are exposed on the insulator surface in the rail gun acceleration hole, and after the projectile passes through that position, a high voltage power source is applied. A method in which a spark is created between the point electrodes, and at the same time, the main power voltage is applied between the rail electrodes, inducing dielectric breakdown between the rail electrodes at that location and starting arc discharge (e.g. R,S,HAWKE,e
t,al,IEEE Transactions on
Magnetics, vol, 25. p219 (198
9))).
上記(11は、簡便な方法ではあるものの、金vI4F
5によるレール電極間の短絡が確実性に乏しく、短絡が
不十分なままでレール電極間に主電源の電圧を荷すると
、レールガンの他の個所で異常放電を起こす可能性があ
る。その対策として、金属箔によるレール電極間の短絡
を検出し、小電源を用いて金属箔を一旦プラズマ化した
後に主ft源の電圧を荷すという方法が報告されている
が(Il、S、HAWKEet、al、IEEE Tr
ansactions on Magnetics、v
ol、Mag22、No、6.p1510(1989)
) 、これは金属箔による短絡を確実化するものではな
く、また複雑な短絡検出回路および付加的電源回路を要
するという欠点がある。Although the above (11) is a simple method, gold vI4F
5, the short circuit between the rail electrodes is not reliable, and if the voltage of the main power source is applied between the rail electrodes while the short circuit is insufficient, there is a possibility that abnormal discharge will occur in other parts of the rail gun. As a countermeasure, a method has been reported in which a short circuit between rail electrodes caused by metal foil is detected, the metal foil is turned into plasma using a small power supply, and then the voltage of the main ft source is applied (Il, S, HAWKEet, al, IEEE Tr.
analyzes on Magnetics, v.
ol, Mag22, No. 6. p1510 (1989)
), which does not ensure short circuits through metal foils and has the disadvantage of requiring complex short circuit detection circuits and additional power supply circuits.
(2)の方法は、飛翔体背面に金属箔等を接着する必要
が無いため、例えば複数の独立したレールガンを連結し
て多段階に電磁加速を行なう場合に、各レールガンにお
けるプラズマ電気子の発生方法としても利用できる。し
かし、+11の場合と同様に付加的な電源回路を必要と
し、またスパークを発生させてから主Ti1l電圧をレ
ール電極間に荷すまでの遅延時間を、精密に制御する必
要がある。さらに、加速孔内に付加的電極が存在するた
め、その位置でのレール電極間の耐電圧が低下し、電磁
加速中に再点弧プラズマが発生する原因になる可能性が
ある。この再点弧プラズマの発生は、電磁加速の効率を
急激に低下させる原因と考えられている。Method (2) does not require the attachment of metal foil or the like to the back surface of the projectile, so when, for example, multiple independent railguns are connected and electromagnetic acceleration is performed in multiple stages, the generation of plasma electrons in each railgun is possible. It can also be used as a method. However, as in the case of +11, an additional power supply circuit is required, and the delay time between generating the spark and applying the main Ti1l voltage across the rail electrodes must be precisely controlled. Furthermore, the presence of additional electrodes in the acceleration hole reduces the withstand voltage between the rail electrodes at that location, which can cause restriking plasma to occur during electromagnetic acceleration. The generation of this restriking plasma is considered to be the cause of the rapid decrease in the efficiency of electromagnetic acceleration.
本発明は、レールガンのプラズマ電機子形成における従
来技術の上記課題を解消して、簡単な回路を用いて、飛
翔体の背後にプラズマ電機子を確実に形成できる方法と
、これを用いたレールガン型tM1加速装置を提供しよ
うとするものである。The present invention solves the above-mentioned problems of the conventional technology in forming a plasma armature for a rail gun, and provides a method for reliably forming a plasma armature behind a flying object using a simple circuit, and a method for forming a rail gun type using this method. The aim is to provide a tM1 accelerator.
前記課題を解決するため、発明者らは鋭意研究を重ねた
結果、本発明をなすに至った。In order to solve the above-mentioned problems, the inventors conducted extensive research and as a result, they came up with the present invention.
すなわち、本発明の構成は、レールガンと、加速電流を
供給するための大電流ti <スイッチングシステム、
クローバ−回路を含む)からなる回路において、新たに
線爆発回路をレールガンと並列に接続して、その線爆発
部を片方のレール電極内部の空洞内に設置し、1isi
t圧が付加されると同時に空洞内に発生する線爆発プラ
ズマをレール電極表面の細孔を通して加速孔内部に吹き
込み、レール電極間の特定の場所にアーク放電を生じさ
せることにより、加速孔内部に付加的な電極を設置する
ことなく、なおかつ付加的な電源及びスイッチングシス
テムを用いることなしに、金X箔等のプラズマ形成材料
があらかじめ存在しない加速孔内の特定の場所にプラズ
マ電機子を形成することを可能にした、レールガンのプ
ラズマ電機子形された線爆発回路の使用により、問題が
解決された0図面を参照して具体的に説明すると、第1
図(81は本発明の代表的な例である。線爆発回路の線
爆発部は金属の細線8で、片方のレール電極内部の空洞
9内に設置され、この細線の一端は空洞内面に接触し、
他端は抵抗体10を介してもう一方のレールに接続され
ている。空洞は細孔11を介して加速孔とつながってい
る。第1図(blのように主電源のスイッチ6を閉じて
電圧をレールガン及び線爆発回路に荷すると、主itt
源からの電流■はまず線爆発回路8.10に流れ、細線
8は線爆発によりプラズマ化する0発生したプラズマ1
2は細孔を通って加速孔内へ高速に吹き込まれ、それと
同時に線爆発回路両端の電圧がレール電極間に荷せられ
る。That is, the configuration of the present invention includes a railgun, a large current ti<switching system for supplying an accelerating current,
In the circuit consisting of a crowbar circuit), a new wire explosion circuit is connected in parallel with the rail gun, and its wire explosion section is installed in the cavity inside one of the rail electrodes, and 1isi
At the same time as the t pressure is applied, the line explosion plasma generated in the cavity is blown into the acceleration hole through the pores on the surface of the rail electrode, causing an arc discharge at a specific location between the rail electrodes. Forming a plasma armature at a specific location within the acceleration hole where no plasma-forming material, such as gold-X foil, is pre-existing, without installing additional electrodes and without using additional power supplies and switching systems. The problem was solved by the use of the rail gun's plasma armature-shaped line detonation circuit, which made it possible to
Figure (81) is a typical example of the present invention. The wire explosion part of the wire explosion circuit is a thin metal wire 8 installed in a cavity 9 inside one of the rail electrodes, and one end of this thin wire is in contact with the inner surface of the cavity. death,
The other end is connected to the other rail via a resistor 10. The cavity is connected to the acceleration hole via the pore 11. When the main power switch 6 is closed and voltage is applied to the rail gun and wire explosion circuit as shown in Figure 1 (bl), the main itt
The current ■ from the source first flows to the wire explosion circuit 8.10, and the thin wire 8 becomes plasma due to the wire explosion.
2 is blown into the acceleration hole through the pore at high speed, and at the same time the voltage across the wire detonation circuit is applied between the rail electrodes.
吹き込まれたプラズマの先端が加速孔内の反対側のレー
ル電極面に到達するとレールtitFfA間の絶縁が破
壊され、第1図tc+のように主7:Xiiからの電流
は線爆発回路からレール電極間のアーク放電へと急速に
移行し、このアーク放電プラズマ13は1を磁力を受け
て加速されプラズマ電機子としての役割を果たすように
なる。411!爆発回路に通電を開始してからレール電
極間のアーク放電が発生するまでの遅延時間は本発明に
とって重要な特性であり、線爆発部の細線の直径、空洞
の容積、細孔の直径に大きく依存する。この遅延時間は
]OI3以下が要求され、そのため線爆発回路の細線と
しては直径0.1 m程度の金属細線、空洞の容積は数
n’、また細孔の直径は1〜21が望ましい、また線爆
発回路両端に発生する電圧は、上記の遅延時間のみなら
ずアーク放電開始後の線爆発回路を流のアークT!1流
への移行速度にとって重要であり、500 V以上3k
V以下が要求される。そのため線爆発回路の抵抗体とし
ては数百mΩが望ましい。When the tip of the injected plasma reaches the rail electrode surface on the opposite side inside the acceleration hole, the insulation between the rails titFfA is broken, and the current from main 7: This arc discharge plasma 13 is accelerated by the magnetic force of 1 and comes to play the role of a plasma armature. 411! The delay time from the start of energization to the detonation circuit to the occurrence of arc discharge between the rail electrodes is an important characteristic for the present invention, and it depends greatly on the diameter of the thin wire in the wire detonation part, the volume of the cavity, and the diameter of the pores. Dependent. This delay time is required to be less than OI3, and therefore the thin wire of the wire explosion circuit is preferably a thin metal wire with a diameter of about 0.1 m, the volume of the cavity is several n', and the diameter of the pore is preferably 1 to 21. The voltage generated across the wire explosion circuit is determined not only by the above delay time but also by the arc T! Important for the transition speed to the first stream, 500 V or more 3k
V or less is required. Therefore, it is desirable that the resistance of the wire explosion circuit be several hundred mΩ.
以下、実施例によって本発明を具体的に説明する。 Hereinafter, the present invention will be specifically explained with reference to Examples.
第1図(δ)に示す方法において、全長駒300fiの
レールガンと6kVに充電された1500μFのキャパ
シターバンクを用いてプラズマ電機子の形成実験を行な
った。線爆発部として直径0.1mの銅細線を、抵抗体
として200mΩを用いた。細孔の直径は1,5fl、
空洞部の体積は細孔を含めて約5鶴3である。両レール
電極間の距離は14鶴である。キャパシターの放[電流
とvA爆発回路電流をそれぞれ独立に測定し、またレー
ルガン内部におけるプラズマ電機子の形成および加速の
様子は、プラズマからの発光を加速孔に沿って設置され
た光プローブを用いて観測することにより評価した。In the method shown in FIG. 1 (δ), a plasma armature formation experiment was conducted using a rail gun with a total length of 300 fi and a 1500 μF capacitor bank charged to 6 kV. A thin copper wire with a diameter of 0.1 m was used as the wire explosion part, and a resistance of 200 mΩ was used as the resistor. The diameter of the pore is 1.5fl,
The volume of the cavity including the pores is approximately 5.3 mm. The distance between both rail electrodes is 14 squares. The discharge current of the capacitor and the vA detonation circuit current were measured independently, and the formation and acceleration of the plasma armature inside the rail gun was measured using an optical probe installed along the acceleration hole to measure the light emission from the plasma. Evaluation was made by observation.
その結果、第2図に示すような結果が得られた。As a result, the results shown in FIG. 2 were obtained.
放電開始とともに全電流14はまず線爆発回路に流れ、
[1発によって発生したプラズマは細孔を通って加速孔
内に吹き込まれる。この現象は細孔付近に設置された光
プローブからの信号16の初期の小さなピークから確認
できる。約10 as後、電流債が約20kAに達した
時点でレール電極間の細孔のある場所で新たなアーク放
電が発生し、それとともに線爆発回路の電流は急速に減
衰し、全電流はアーク放電を流へ急速に移行する。各位
1の光プローブ信号16.17.18,19.20から
れかるように、アーク放電プラズマは約2.5〜3.0
km / sの速度で移動するプラズマ電機子になって
いることがわかる。When the discharge starts, the entire current 14 first flows into the wire explosion circuit,
[The plasma generated by one shot is blown into the acceleration hole through the pore. This phenomenon can be confirmed from the initial small peak of the signal 16 from the optical probe placed near the pore. After about 10 as, when the current reaches about 20 kA, a new arc discharge occurs at the location of the pore between the rail electrodes, and with it the current in the line detonation circuit rapidly decays, and the total current is reduced to arc Rapidly transitions discharge to current. As can be seen from the optical probe signals 16.17.18 and 19.20, the arc discharge plasma is about 2.5~3.0
It can be seen that it is a plasma armature moving at a speed of km/s.
以上説明したようにレールガンと並列に接続された線爆
発回路を使用する本発明の方法により、プラズマ形成材
料が存在しないレールガン加速孔内に、付加的な電極や
付加的な[fi及びスイッチシステムを用いることなく
、容易、かつ再現性がきわめて良好にプラズマ電機子の
形成を行なうことができる。又、本発明は複数のレール
ガンを用いて多段の電磁加速を行なう場合において、各
し一ルガンのプラズマ1ifIi子の形成方法及びこれ
を用いたレールガン型iitM!L加速装置としても有
効に利用できるものである。As described above, the method of the present invention using a wire detonation circuit connected in parallel with the railgun allows the addition of additional electrodes and additional [fi and switch systems] into the railgun acceleration hole where no plasma-forming material is present. Plasma armatures can be formed easily and with extremely good reproducibility without the use of a plasma armature. Further, the present invention provides a method for forming a plasma 1ifIi of one railgun each, and a railgun type iitM! It can also be effectively used as an L accelerator.
第1図(a) 、 (bl 、 (c)は、本発明の詳
細な説明す撮
るための模式図、第2図は実施例の結果を示す売F図
わであり、第3図(al、(blは従来の技術を説明す
るための模式図である。
l:レール電極、2:加速孔、3:飛翔体、4:プラズ
マ形成材料、5:主1tS、6:スイッチ、7:プラズ
マ電機子、8:線場発部の金属細線、9:空洞、10:
抵抗体、11:細孔、12:線爆発プラズマ、13:ア
ーク放電プラズマ (プラズマ電気子)、14:全電流
、15:線爆発回路i流、16〜20:各光プローブか
らの信号。
代理人frJx士 山 口 JL i’−、’、シ
\′−;゛
、1ノ1.”−1−ノ
第 1. 7
T1−糧II+!−bs)Figures 1 (a), (bl, and c) are schematic diagrams for taking detailed explanations of the present invention, Figure 2 is a sales diagram showing the results of examples, and Figure 3 (al , (bl is a schematic diagram for explaining the conventional technology. l: rail electrode, 2: acceleration hole, 3: flying object, 4: plasma forming material, 5: main 1tS, 6: switch, 7: plasma Armature, 8: Fine metal wire at the line field source, 9: Cavity, 10:
Resistor, 11: Pore, 12: Line explosion plasma, 13: Arc discharge plasma (plasma electron), 14: Total current, 15: Line explosion circuit i current, 16 to 20: Signals from each optical probe. Agent frJx person Yamaguchi JL i'-,', shi\'-;゛, 1 no 1. ”-1-No. 1.7 T1-Summary II+!-bs)
Claims (1)
ための大電流電源(スイッチングシステム、クローバー
回路を含む)からなる回路において、新たに線爆発回路
をレールガン型電磁加速装置と並列に接続して、その線
爆発部を片方のレール電極内部の空洞内に設置し、電源
電圧が付加されると同時に空洞内に発生する線爆発プラ
ズマをレール電極表面の細孔を通して加速孔内部に吹き
込み、レール電極間の特定の場所にアーク放電を生じさ
せることにより、金属箔等のプラズマ形成材料があらか
じめ存在しない加速孔内の特定の場所に、プラズマ電機
子を形成することを特徴とする、レールガン型電磁加速
装置のプラズマ電機子形成方法。 2)加速電流を供給する大電流電源を有するレールガン
型電磁加速装置において、この電磁加速装置が、レール
ガン型電磁加速装置と並列に接続され、いずれか一方の
レール電極内部の空洞内に設けられ電源電圧の付加によ
り加速孔内にプラズマ電機子を形成させる線爆発部とか
らなる線爆発回路を備えたことを特徴とするレールガン
型電磁加速装置。[Claims] 1) In a circuit consisting of a railgun type electromagnetic accelerator and a large current power supply (including a switching system and a crowbar circuit) for supplying acceleration current, a line explosion circuit is newly added to the railgun type electromagnetic accelerator. The line explosion part is installed in the cavity inside one of the rail electrodes, and when the power supply voltage is applied, the line explosion plasma generated in the cavity passes through the pores on the surface of the rail electrode and accelerates into the hole. It is characterized by forming a plasma armature at a specific location within the acceleration hole where no plasma-forming material such as metal foil already exists by blowing into the inside and causing an arc discharge at a specific location between the rail electrodes. A method for forming a plasma armature for a railgun type electromagnetic accelerator. 2) In a rail gun type electromagnetic accelerator having a large current power source that supplies an accelerating current, this electromagnetic accelerator is connected in parallel with the rail gun type electromagnetic accelerator, and is provided in a cavity inside one of the rail electrodes and has a power source. A rail gun type electromagnetic accelerator characterized by comprising a line explosion circuit consisting of a line explosion section that forms a plasma armature within an acceleration hole by applying voltage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2102401A JP2571862B2 (en) | 1990-04-18 | 1990-04-18 | Method and apparatus for forming plasma armature of railgun type electromagnetic accelerator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2102401A JP2571862B2 (en) | 1990-04-18 | 1990-04-18 | Method and apparatus for forming plasma armature of railgun type electromagnetic accelerator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH043896A true JPH043896A (en) | 1992-01-08 |
| JP2571862B2 JP2571862B2 (en) | 1997-01-16 |
Family
ID=14326426
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2102401A Expired - Lifetime JP2571862B2 (en) | 1990-04-18 | 1990-04-18 | Method and apparatus for forming plasma armature of railgun type electromagnetic accelerator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2571862B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10278761B2 (en) | 2011-02-28 | 2019-05-07 | Ethicon Llc | Electrical ablation devices and methods |
-
1990
- 1990-04-18 JP JP2102401A patent/JP2571862B2/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10278761B2 (en) | 2011-02-28 | 2019-05-07 | Ethicon Llc | Electrical ablation devices and methods |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2571862B2 (en) | 1997-01-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3103861B2 (en) | Sabo separation device for flying object accelerator | |
| MacGregor et al. | The influence of polarity on trigatron switching performance | |
| CN115681052B (en) | Hall thruster, equipment with same and use method of Hall thruster | |
| WO2024254292A1 (en) | Magnetoplasmadynamic thruster with reverse polarity and tailored mass flux | |
| JPH043896A (en) | Method and device for forming plasma armature of rail gun type electromagnetic accelerator | |
| Ge et al. | Analysis and research on muzzle arc suppression device of arc striking railgun | |
| JP2571863B2 (en) | Railgun type electromagnetic accelerator with distributed electrodes | |
| Zhou et al. | Study on arc behaviors at opening a 270V resistive circuit by bridge-type contacts under magnetic field | |
| US4706542A (en) | Low voltage arc formation in railguns | |
| Tamura et al. | Laser‐prearc railgun: Development for the application to a fuel pellet injector of a nuclear fusion reactor | |
| Petr et al. | Erosion of spark gap electrodes | |
| Hachiman et al. | Study on small DC vacuum arc characteristic under transverse magnetic field | |
| Pushkarev et al. | Stabilization of ion beam generation in a diode with self-magnetic insulation in double-pulse mode | |
| Moschella et al. | An inverse pinch plasma source for plasma opening switches | |
| JP2923100B2 (en) | Railgun for fusion pellet injector | |
| US3441798A (en) | Plasma gun utilizing successive arcs for generating and accelerating the plasma | |
| Teste et al. | General properties of high current switching under 36 V DC for Ag and AgSnO2 contacts | |
| US10278276B2 (en) | Short pulse neutron generator | |
| Ashby et al. | Quasi-steady-state pulsed plasma thrusters. | |
| RU2398350C1 (en) | Method of generating current pulse for liner acceleration with pulsed source magnetic field | |
| JP6994617B2 (en) | Electromagnetic projectile accelerator | |
| Khvorost et al. | The role of emission properties in non-sustained disruptive discharge (NSDD) evolution | |
| Karhi et al. | Analysis of distributed energy railguns to suppress secondary arc formation | |
| SU784721A1 (en) | Ion accelerator | |
| US20160054093A1 (en) | Electromagnetic device and method to accelerate solid metal slugs to high speeds |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| S111 | Request for change of ownership or part of ownership |
Free format text: JAPANESE INTERMEDIATE CODE: R313117 |
|
| S533 | Written request for registration of change of name |
Free format text: JAPANESE INTERMEDIATE CODE: R313533 |
|
| R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
| EXPY | Cancellation because of completion of term |