JPH0229899U - - Google Patents

Info

Publication number
JPH0229899U
JPH0229899U JP10838288U JP10838288U JPH0229899U JP H0229899 U JPH0229899 U JP H0229899U JP 10838288 U JP10838288 U JP 10838288U JP 10838288 U JP10838288 U JP 10838288U JP H0229899 U JPH0229899 U JP H0229899U
Authority
JP
Japan
Prior art keywords
tether
satellite
rollers
roller support
support body
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
Application number
JP10838288U
Other languages
Japanese (ja)
Other versions
JPH0735840Y2 (en
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 filed Critical
Priority to JP10838288U priority Critical patent/JPH0735840Y2/en
Publication of JPH0229899U publication Critical patent/JPH0229899U/ja
Application granted granted Critical
Publication of JPH0735840Y2 publication Critical patent/JPH0735840Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Placing Or Removing Of Piles Or Sheet Piles, Or Accessories Thereof (AREA)
  • Radio Relay Systems (AREA)

Description

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

第１図ないし第５図はこの考案のテザー衛星用
テザーガイド装置の一実施例を示す図で、第１図
は同装置の要部を示す断面図、第２図は第１図の
右側面図、第３図および第４図はテザー衛星や格
子状ブーム等を示す図で、第３図はテザー衛星格
納状態を、又、第４図はテザー衛星吊下げ状態を
示す斜視図、第５図は同装置のブロツク図、第６
図ないし第８図は従来例を示す図で、第６図は母
船衛星並びにテザー衛星を示す斜視図、第７図は
両衛星が地球の回りを周回している状態を示す概
略図、第８図は主にテザーとローラとの関係を示
す斜視図である。 １２……母船衛星側テザー装置、１３……地球
（天体）、１４……テザー、１５……テザー衛星
、１８……テザーガイド装置、２１……ローラ支
持体、２２……ローラ、２４……駆動歯車、２５
……モータ、駆動手段、２６……制御装置。 Figures 1 to 5 are diagrams showing an embodiment of the tether guide device for tethered satellites of this invention. Figure 1 is a sectional view showing the main parts of the device, and Figure 2 is the right side of Figure 1. Figures 3 and 4 are views showing the tethered satellite, lattice boom, etc. Figure 3 is a perspective view showing the tethered satellite in the stored state, Figure 4 is a perspective view showing the tethered satellite in the suspended state, and Figure 5 is a perspective view showing the tethered satellite in the suspended state. The figure is a block diagram of the same device, No. 6
Figures 8 through 8 are diagrams showing the conventional example. Figure 6 is a perspective view showing a mother satellite and a tether satellite, Figure 7 is a schematic diagram showing both satellites orbiting around the earth, and Figure 8 is a diagram showing a state where both satellites are orbiting around the earth. The figure is a perspective view mainly showing the relationship between the tether and the rollers. 12... Mother ship satellite side tether device, 13... Earth (celestial body), 14... Tether, 15... Tether satellite, 18... Tether guide device, 21... Roller support, 22... Roller, 24... Drive gear, 25
...Motor, drive means, 26...Control device.

Claims (1)

【実用新案登録請求の範囲】 天体の回りを一定の姿勢を保つて周回する母船
衛星に、テザーを引出し・巻取り自在とするコン
トロール装置が設けられ、該テザーを一対のロー
ラの間に挾持して案内することにより、該テザー
の先端部に取付けられたテザー衛星を前記母船衛
星から前記ローラの軸方向と直交する方向に吊り
下げるテザーガイド装置において、 前記一対のローラを内部に回転自在に支持する
ローラ支持体を、前記吊下げ方向と略直交する方
向を中心に回転自在となるように配設すると共に
、該ローラ支持体を回転させる駆動手段を設け、
該駆動手段を制御して、前記母船衛星が前記天体
を周回する角速度と同期して前記ローラ支持体を
回転させて前記ローラ軸を吊り下げ方向と常に略
直交させる制御装置を設けたことを特徴とするテ
ザー衛星用テザーガイド装置。[Claim for Utility Model Registration] A mother satellite that orbits around a celestial body while maintaining a constant attitude is provided with a control device that allows the tether to be freely pulled out and retracted, and the tether is held between a pair of rollers. A tether guide device that suspends a tethered satellite attached to the tip of the tether from the mother satellite in a direction perpendicular to the axial direction of the rollers, the pair of rollers being rotatably supported inside. A roller support body is disposed so as to be freely rotatable around a direction substantially perpendicular to the hanging direction, and a driving means for rotating the roller support body is provided,
A control device is provided which controls the drive means to rotate the roller support body in synchronization with the angular velocity at which the mother satellite orbits the celestial body, so that the roller axis is always substantially perpendicular to the hanging direction. A tether guide device for tethered satellites.
JP10838288U 1988-08-18 1988-08-18 Tether guide device for tether satellite Expired - Lifetime JPH0735840Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10838288U JPH0735840Y2 (en) 1988-08-18 1988-08-18 Tether guide device for tether satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10838288U JPH0735840Y2 (en) 1988-08-18 1988-08-18 Tether guide device for tether satellite

Publications (2)

Publication Number Publication Date
JPH0229899U true JPH0229899U (en) 1990-02-26
JPH0735840Y2 JPH0735840Y2 (en) 1995-08-16

Family

ID=31343656

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10838288U Expired - Lifetime JPH0735840Y2 (en) 1988-08-18 1988-08-18 Tether guide device for tether satellite

Country Status (1)

Country Link
JP (1) JPH0735840Y2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06225660A (en) * 1993-02-01 1994-08-16 Azuma Corp:Kk Water-feeder for bird breeding

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4543203B2 (en) * 2005-11-10 2010-09-15 独立行政法人 宇宙航空研究開発機構 Space tether

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06225660A (en) * 1993-02-01 1994-08-16 Azuma Corp:Kk Water-feeder for bird breeding

Also Published As

Publication number Publication date
JPH0735840Y2 (en) 1995-08-16

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