JPH0244600U - - Google Patents
Info
- Publication number
- JPH0244600U JPH0244600U JP12447588U JP12447588U JPH0244600U JP H0244600 U JPH0244600 U JP H0244600U JP 12447588 U JP12447588 U JP 12447588U JP 12447588 U JP12447588 U JP 12447588U JP H0244600 U JPH0244600 U JP H0244600U
- Authority
- JP
- Japan
- Prior art keywords
- paddle
- satellite
- built
- paddles
- solar array
- 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
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Photovoltaic Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図及び第２図はこの考案の一実施例を示す
三軸姿勢制御型人工衛星の外観図、第２図は太陽
電池パドル展開後の状態を示す図、第３図は従来
の例を示す三軸姿勢制御型人工衛星の外観図、第
４図、第５図、第６図は従来の例を示す三軸姿勢
制御型人工衛星の太陽電池パドルの展開方法を段
階毎に示す図である。
図において、１は人工衛星本体、２は合成開口
レーダ、３は円筒スライド式太陽電池パドル、４
ａ，４ｂ，４ｃは衛星座標の定義、５は従来の太
陽電池パドル、６はヒンジ、７はパドル回転方向
を示す。なお、図中、同一符号は同一または相当
部分を示す。
Figures 1 and 2 are external views of a three-axis attitude control artificial satellite that shows one embodiment of this invention, Figure 2 shows the state after the solar array paddles are deployed, and Figure 3 shows a conventional example. Figures 4, 5, and 6 are diagrams showing, step by step, the method of deploying the solar array paddles of a conventional three-axis attitude control satellite. be. In the figure, 1 is the satellite body, 2 is the synthetic aperture radar, 3 is the cylindrical sliding solar array paddle, and 4 is the synthetic aperture radar.
a, 4b, and 4c are definitions of satellite coordinates, 5 is a conventional solar array paddle, 6 is a hinge, and 7 is a paddle rotation direction. In addition, in the figures, the same reference numerals indicate the same or corresponding parts.
Claims (1)
電池パドルにおいて、一枚のパドルに複数のパド
ルを内蔵し、その内蔵されたパドルをスライドし
、太陽光より大電力を得る円筒スライド式の太陽
電池パドルを備え、人工衛星の位置にかかわらず
太陽光を受けることのできる形状にしたことを特
徴とする人工衛星の太陽電池パドル。 A solar array paddle that supplies power to a three-axis attitude control satellite has multiple paddles built into one paddle, and the built-in paddles are slid to generate a large amount of power from sunlight. A solar battery paddle for an artificial satellite, which is equipped with a battery paddle and has a shape that allows it to receive sunlight regardless of the position of the satellite.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12447588U JPH0244600U (en) | 1988-09-22 | 1988-09-22 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12447588U JPH0244600U (en) | 1988-09-22 | 1988-09-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0244600U true JPH0244600U (en) | 1990-03-27 |
Family
ID=31374240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12447588U Pending JPH0244600U (en) | 1988-09-22 | 1988-09-22 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0244600U (en) |
-
1988
- 1988-09-22 JP JP12447588U patent/JPH0244600U/ja active Pending
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