JPS60103100U - spin-stabilized satellite - Google Patents
spin-stabilized satelliteInfo
- Publication number
- JPS60103100U JPS60103100U JP19555783U JP19555783U JPS60103100U JP S60103100 U JPS60103100 U JP S60103100U JP 19555783 U JP19555783 U JP 19555783U JP 19555783 U JP19555783 U JP 19555783U JP S60103100 U JPS60103100 U JP S60103100U
- Authority
- JP
- Japan
- Prior art keywords
- satellite
- panels
- spin
- panel device
- buffer material
- 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ａ、 ｂはそれぞれ太陽電池の代表的室−圧■−
電電流性特性および同発生電力の代表的経年劣化特性を
示す図、第３図は従来のスピン安定型人工衛星の打上げ
ロケット搭載状況図、第４図ａ、 ｂはそれぞれこの考
案の一実施例を示す外観図、同下方面直視図、第５図は
第４図要部の拡大断面図、第６図はこの考案の衛星の打
上げロケット搭載状況図、第７図はこの考案の衛星の付
加パネル展開までの概略例を静止衛星について示した図
である。
図において、１０は衛星、１１は太陽電池付加展開パネ
ル、１２は受は材、１３は爆破装置、１４は固定用り字
形ボルト、１５はヒンジ、１６゜１７はスプリング、１
８は緩衝体、１９はケース・ −ルである。なお、各
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７−図□ Figure 1 is an external view of a conventional spin-stabilized communication satellite.
Figures 2a and b are representative chambers of solar cells - pressure -
Figure 3 is a diagram showing the current characteristics and typical aging characteristics of the generated power. Figure 3 is a diagram of a conventional spin-stabilized artificial satellite mounted on a launch vehicle, and Figures 4 a and b are examples of this invention. Fig. 5 is an enlarged sectional view of the main part of Fig. 4, Fig. 6 is a diagram of the launch vehicle mounted on the satellite of this invention, and Fig. 7 is an addition to the satellite of this invention. FIG. 2 is a diagram showing a schematic example of a geostationary satellite up to panel development. In the figure, 10 is a satellite, 11 is a solar cell additional expansion panel, 12 is a support material, 13 is an explosive device, 14 is a fixing bolt, 15 is a hinge, 16° and 17 are springs, 1
8 is a buffer body, and 19 is a case rule. Note that the same reference numerals in each figure indicate the same or corresponding parts. -( Figure 7-
Claims (1)
星本体下部の同心円上に取付けられたヒンジに回動自在
に結合し、また他端は略り字形部材を介して衛星本体に
設けた切り離し機構に結合して衛星本体外周面を覆い、
かつ上記切り離し機構で上記路り字形部材を衛星本体か
ら切り離すことにより上記複数のパネルを展開する太陽
電池パネル装置と、上記衛星本体下部に設けられ、上記
展開した複数のパネルと嵌合し、固定する緩衝体材受は
材とを具備したことを特徴とするスピン安定型人工衛星
。One end of each of the plurality of panels provided with solar cells is rotatably connected to a hinge mounted on a concentric circle at the bottom of the satellite body, and the other end is connected to a separation mechanism provided on the satellite body via an abbreviated member. to cover the outer surface of the satellite body,
and a solar cell panel device that deploys the plurality of panels by separating the road-shaped member from the satellite main body with the separation mechanism, and a solar panel device that is provided at the lower part of the satellite main body and that fits and fixes the plurality of panels that have been developed. A spin-stabilized artificial satellite characterized by comprising a buffer material holder and a buffer material holder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19555783U JPS60103100U (en) | 1983-12-20 | 1983-12-20 | spin-stabilized satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP19555783U JPS60103100U (en) | 1983-12-20 | 1983-12-20 | spin-stabilized satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS60103100U true JPS60103100U (en) | 1985-07-13 |
Family
ID=30419925
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP19555783U Pending JPS60103100U (en) | 1983-12-20 | 1983-12-20 | spin-stabilized satellite |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60103100U (en) |
-
1983
- 1983-12-20 JP JP19555783U patent/JPS60103100U/en active Pending
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