JPS60170300U - spin-stabilized satellite - Google Patents
spin-stabilized satelliteInfo
- Publication number
- JPS60170300U JPS60170300U JP5948184U JP5948184U JPS60170300U JP S60170300 U JPS60170300 U JP S60170300U JP 5948184 U JP5948184 U JP 5948184U JP 5948184 U JP5948184 U JP 5948184U JP S60170300 U JPS60170300 U JP S60170300U
- Authority
- JP
- Japan
- Prior art keywords
- spin
- satellite
- cell array
- solar cell
- stabilized
- 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
Links
Landscapes
- Photovoltaic Devices (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
第１図は従来のスピン安定型通信衛星の外観図、第２図
は、太陽電池アレイの代表的電圧■−電電流性特性図第
３図はこの考案の一実施例を示す外観図、第４図は、第
３図のノズル側からの直視図、第５図ａ、 ｂは第４図
の状態からそれぞれ −外層側の太陽電池アレイパネ
ルの拡張した状態図、内層側の太陽電池アレイパネルを
も拡張した状態図、第６図は拡張機構の一実施例図であ
る。
―において、５は縮小時内層側に位置する４分割で例示
する太陽電池アレイパネル、６は同じく外層側に位置す
る太陽電池アレイパネル、７は衛星本体、８〜１１は拡
張機構の一実施例を構成するモータ、ピニオン、ラック
である。なお、図中同一符号は同一または相当部分を示
すものとする。 ”
第３図 “
第５図Fig. 1 is an external view of a conventional spin-stabilized communication satellite, Fig. 2 is a typical voltage-current characteristic diagram of a solar cell array, and Fig. 3 is an external view of an embodiment of this invention. Figure 4 is a direct view from the nozzle side in Figure 3, and Figures 5a and b are the expanded state diagram of the solar cell array panel on the outer layer side and the solar cell array panel on the inner layer side, respectively. FIG. 6 is a diagram showing an example of the expanding mechanism. -, 5 is a solar cell array panel exemplified by four divisions located on the inner layer side when contracted, 6 is a solar cell array panel also located on the outer layer side, 7 is the satellite body, and 8 to 11 are an example of an expansion mechanism. These are the motor, pinion, and rack that make up the unit. Note that the same reference numerals in the figures indicate the same or corresponding parts. ” Figure 3 “ Figure 5
Claims (1)
同心円状に二層構造で、且つそれぞれ複数分割形の拡張
可能な太陽電池アレイパネルで包覆し、ロケット分離さ
れた軌道上にて同心円状に一層状態になる如く、上記の
パネルを拡張させ、それによって太陽受光面積の増加を
図るように構成したことを特徴とするスピン安定型人工
衛星。In a spin-stabilized artificial satellite, the outer circumferential surface of the satellite body has a two-layered concentric structure, each covered with multiple split expandable solar cell array panels, and concentric circles on the orbit separated by the rocket. A spin-stabilized artificial satellite characterized in that the above-mentioned panel is expanded to further increase the solar light receiving area.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5948184U JPS60170300U (en) | 1984-04-23 | 1984-04-23 | spin-stabilized satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5948184U JPS60170300U (en) | 1984-04-23 | 1984-04-23 | spin-stabilized satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS60170300U true JPS60170300U (en) | 1985-11-12 |
Family
ID=30585949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5948184U Pending JPS60170300U (en) | 1984-04-23 | 1984-04-23 | spin-stabilized satellite |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60170300U (en) |
-
1984
- 1984-04-23 JP JP5948184U patent/JPS60170300U/en active Pending
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