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JPH04218498A - Plasma shielding device for space structure - Google Patents

Plasma shielding device for space structure

Info

Publication number
JPH04218498A
JPH04218498A JP2411426A JP41142690A JPH04218498A JP H04218498 A JPH04218498 A JP H04218498A JP 2411426 A JP2411426 A JP 2411426A JP 41142690 A JP41142690 A JP 41142690A JP H04218498 A JPH04218498 A JP H04218498A
Authority
JP
Japan
Prior art keywords
space structure
plasma
magnet
shielding device
solar wind
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.)
Pending
Application number
JP2411426A
Other languages
Japanese (ja)
Inventor
Moroo Nakayama
師生 中山
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Corp
Original Assignee
Ishikawajima Harima Heavy Industries Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Ishikawajima Harima Heavy Industries Co Ltd filed Critical Ishikawajima Harima Heavy Industries Co Ltd
Priority to JP2411426A priority Critical patent/JPH04218498A/en
Publication of JPH04218498A publication Critical patent/JPH04218498A/en
Pending legal-status Critical Current

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  • Plasma Technology (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は宇宙構造物のプラズマシ
―ルド装置に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a plasma shielding device for a space structure.

【0002】0002

【従来の技術】シャトル、ステ―ション、コロニ―等の
宇宙構造物は常時太陽風に晒されているが、太陽風(プ
ラズマ)は宇宙構造物や該構造物内の人間に悪影響を及
ぼす虞れがある。
[Prior Art] Space structures such as shuttles, stations, and colonies are constantly exposed to solar wind, but solar wind (plasma) can have a negative impact on space structures and the people inside the structures. be.

【0003】0003

【発明が解決しようとする課題】本発明は上述の実情に
鑑み、宇宙構造物がプラズマに晒されないようにするこ
とを目的としてなしたものである。
SUMMARY OF THE INVENTION In view of the above-mentioned circumstances, the present invention has been made with the object of preventing space structures from being exposed to plasma.

【0004】0004

【課題を解決するための手段】本発明は、宇宙構造物の
外部に磁石を設置し、磁石により生じた磁束によりプラ
ズマを磁石の極部近傍に捕集し得るよう構成したもので
ある。
[Means for Solving the Problems] The present invention is configured such that a magnet is installed outside a space structure, and plasma can be collected near the pole of the magnet by the magnetic flux generated by the magnet.

【0005】[0005]

【作用】宇宙構造物に吹き付けられたプラズマは、磁束
に沿いドリフト運動して磁石の極部近傍に捕集され、再
結合して消滅する。
[Operation] Plasma blown onto a space structure drifts along the magnetic flux, is collected near the pole of the magnet, recombines, and disappears.

【0006】[0006]

【実施例】以下、本発明の実施例を添付図面を参照しつ
つ説明する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings.

【0007】図1中1は宇宙構造物、2は宇宙構造物1
の外表面に設置した磁石、3は磁石2により発生する磁
束、4は太陽風(プラズマ)、5は磁石2の各極部2a
近傍に形成されるプラズマ消滅部である。
In FIG. 1, 1 is a space structure, and 2 is a space structure 1.
3 is the magnetic flux generated by the magnet 2, 4 is the solar wind (plasma), 5 is each pole part 2a of the magnet 2
This is a plasma extinguishing section formed nearby.

【0008】太陽風4は、プロトンH+や電子e−がプ
ラズマ状態になっているものである。このため太陽風4
が宇宙構造物1に接近すると、プロトンや電子が磁石2
の磁力によって捕促され、磁束3に沿ってドリフト運動
を行い、磁石2の極部に捕集される。換言すれば、磁束
3は地球の地磁気圏と同様の機能を果す。
The solar wind 4 is composed of protons H+ and electrons e- in a plasma state. Therefore, solar wind 4
When approaching space structure 1, protons and electrons are attracted to magnet 2.
is captured by the magnetic force of the magnet, performs a drift motion along the magnetic flux 3, and is captured at the pole of the magnet 2. In other words, the magnetic flux 3 performs a similar function to the earth's magnetosphere.

【0009】而して、プロトンや電子が磁石2極部に捕
集され、プロトンや電子の密度が高くなると、プロトン
と電子が結合して水素分子化する。このため、太陽風4
が宇宙構造物1や宇宙構造物1内の人間に作用すること
がなく、宇宙構造物1が劣化したり、或いは人間が太陽
風4を浴びることにより生じる弊害が防止される。
[0009] When protons and electrons are collected at the two poles of the magnet and the density of the protons and electrons increases, the protons and electrons combine to form hydrogen molecules. For this reason, solar wind 4
does not act on the space structure 1 or the people inside the space structure 1, and harmful effects caused by deterioration of the space structure 1 or exposure of humans to the solar wind 4 are prevented.

【0010】又、プロトンと電子が結合すると、磁石2
の極部には、プラズマ消滅部5が形成され、プラズマ消
滅部5には水素ガスが残留する。
[0010] Also, when protons and electrons combine, the magnet 2
A plasma extinguishing part 5 is formed at the extreme part of the plasma extinguishing part 5, and hydrogen gas remains in the plasma extinguishing part 5.

【0011】この水素ガスは宇宙構造物1に積極的に取
り込み姿勢制御用ガスとして使用することができる。
[0011] This hydrogen gas can be actively taken into the space structure 1 and used as an attitude control gas.

【0012】更に、プロトンと電子が結合する際には、
オ―ロラが発生するため、このオ―ロラを観測し研究す
ることもできる。
Furthermore, when protons and electrons combine,
Since the aurora is generated, it is also possible to observe and study this aurora.

【0013】なお、本発明の実施例では、プラズマとし
て太陽風を例にとり説明したが、プラズマ状になってい
れば太陽風以外の宇宙線に対して適用することもできる
こと、その他、本発明の要旨を逸脱しない範囲内で種々
変更を加え得ること、等は勿論である。
[0013] In the embodiments of the present invention, solar wind was used as an example of plasma for explanation, but the present invention can also be applied to cosmic rays other than solar wind as long as they are in the form of plasma. Of course, various changes may be made within the scope.

【0014】[0014]

【発明の効果】本発明の宇宙構造物のプラズマシ―ルド
装置によれば、宇宙構造物や宇宙構造物内の人間がプラ
ズマに晒されることがなくなるため、安全性が向上する
という優れた効果を奏し得る。
[Effects of the Invention] According to the plasma shield device for a space structure of the present invention, the space structure and the people inside the space structure are not exposed to plasma, so it has the excellent effect of improving safety. It can be played.

【図面の簡単な説明】[Brief explanation of the drawing]

【図1】本発明の宇宙構造物のプラズマシ―ルド装置の
概念を示す平面図である。
FIG. 1 is a plan view showing the concept of a plasma shield device for a space structure according to the present invention.

【符号の説明】[Explanation of symbols]

1    宇宙構造物 2    磁石 2a  極部 3    磁束 4    太陽風(プラズマ) 1 Space structures 2 Magnet 2a Extreme part 3 Magnetic flux 4. Solar wind (plasma)

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】  宇宙構造物の外部に磁石を設置し、磁
石により生じた磁束によりプラズマを磁石の極部近傍に
捕集し得るよう構成したことを特徴とする宇宙構造物の
プラズマシ―ルド装置。
[Claim 1] A plasma shielding device for a space structure, characterized in that a magnet is installed outside the space structure, and the plasma is collected near the pole of the magnet by the magnetic flux generated by the magnet. .
JP2411426A 1990-12-18 1990-12-18 Plasma shielding device for space structure Pending JPH04218498A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2411426A JPH04218498A (en) 1990-12-18 1990-12-18 Plasma shielding device for space structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2411426A JPH04218498A (en) 1990-12-18 1990-12-18 Plasma shielding device for space structure

Publications (1)

Publication Number Publication Date
JPH04218498A true JPH04218498A (en) 1992-08-10

Family

ID=18520438

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2411426A Pending JPH04218498A (en) 1990-12-18 1990-12-18 Plasma shielding device for space structure

Country Status (1)

Country Link
JP (1) JPH04218498A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007043955A1 (en) * 2007-09-14 2009-04-09 Thales Electron Devices Gmbh Device for reducing the impact of a surface area by positively charged ions and ion accelerator arrangement
CN102361797A (en) * 2009-03-26 2012-02-22 科学技术设备委员会 spacecraft protection
DE102017123397B3 (en) * 2017-10-09 2018-06-28 Airbus Defence and Space GmbH Passive protection against radiation

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007043955A1 (en) * 2007-09-14 2009-04-09 Thales Electron Devices Gmbh Device for reducing the impact of a surface area by positively charged ions and ion accelerator arrangement
WO2009037197A3 (en) * 2007-09-14 2009-08-13 Thales Electron Devices Gmbh Device for reducing the impact of positively charged ions on a surface section and ion accelerator arrangement
DE102007043955B4 (en) * 2007-09-14 2010-07-22 Thales Electron Devices Gmbh Device for reducing the impact of a surface area by positively charged ions and ion accelerator arrangement
JP2010539375A (en) * 2007-09-14 2010-12-16 ターレス エレクトロン デバイス ゲゼルシャフト ミット ベシュレンクテル ハフツング Apparatus for reducing the application of positively charged ions to a surface portion, and ion accelerator
RU2472965C2 (en) * 2007-09-14 2013-01-20 Тейлз Электрон Дивайсез Гмбх Ion accelerator with device for reducing effect of positively charged ions on surface area
US8944385B2 (en) 2007-09-14 2015-02-03 Thales Electronic Systems Gmbh Device for reducing the impact on a surface section by positively charged ions, and ion accelelerator arrangement
KR101525150B1 (en) * 2007-09-14 2015-06-03 탈레스 일렉트로닉 시스템즈 게엠베하 Device for reducing the impact of positively charged ions on a surface section and ion accelerator arrangement
CN102361797A (en) * 2009-03-26 2012-02-22 科学技术设备委员会 spacecraft protection
DE102017123397B3 (en) * 2017-10-09 2018-06-28 Airbus Defence and Space GmbH Passive protection against radiation

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