JPH03109999U - - Google Patents
Info
- Publication number
- JPH03109999U JPH03109999U JP1865990U JP1865990U JPH03109999U JP H03109999 U JPH03109999 U JP H03109999U JP 1865990 U JP1865990 U JP 1865990U JP 1865990 U JP1865990 U JP 1865990U JP H03109999 U JPH03109999 U JP H03109999U
- Authority
- JP
- Japan
- Prior art keywords
- artificial satellite
- solar
- satellite
- solar absorption
- attached
- 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
- 238000010521 absorption reaction Methods 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims description 2
- 238000004381 surface treatment Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Photovoltaic Devices (AREA)
- Control Of Temperature (AREA)
Description
第１図はこの考案の人工衛星の一実施例を示す
図、第２図は第１図の一部を太陽光照射２１方向
から見た図、第３図はこの考案の人工衛星に搭載
される電子機器の一年間の温度推移を示す図、第
４図は従来の人工衛星の一実施例を示す図、第５
図は従来の人工衛星に搭載される電子機器の一年
間の温度推移を示す図である。
図において、３……衛星本体、７……太陽電池
パドル、８……フレーム、９……熱放射板、１０
……太陽光吸収率及び赤外放射率が大きい面、１
１……太陽光吸収率が小さい面、１２……駆動用
モータである。なお、図中同一符号は同一または
相当部分を示す。
Figure 1 is a diagram showing an embodiment of the artificial satellite of this invention, Figure 2 is a view of a part of Figure 1 viewed from the direction of sunlight irradiation, and Figure 3 is mounted on the artificial satellite of this invention. Figure 4 is a diagram showing an example of a conventional artificial satellite;
The figure shows the temperature changes over one year of electronic equipment mounted on a conventional artificial satellite. In the figure, 3...Satellite main body, 7...Solar battery paddle, 8...Frame, 9...Heat radiation plate, 10
...Surface with high solar absorption and infrared emissivity, 1
1... Surface with low solar absorption rate, 12... Drive motor. Note that the same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
星において、片面は太陽光吸収率及び赤外放射率
が大きく他面は太陽光吸収率が小さい表面処理を
施した熱放射板を、太陽電池パドルのフレームに
回転する様に駆動モータを介して取付けたことを
特徴とする人工衛星。 In an artificial satellite consisting of a satellite body and a solar array paddle, a heat radiation plate with a surface treatment that has high solar absorption and infrared emissivity on one side and low solar absorption on the other side is attached to the frame of the solar array paddle. An artificial satellite characterized by being attached via a drive motor so that it rotates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1865990U JPH03109999U (en) | 1990-02-26 | 1990-02-26 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1865990U JPH03109999U (en) | 1990-02-26 | 1990-02-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03109999U true JPH03109999U (en) | 1991-11-12 |
Family
ID=31521811
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1865990U Pending JPH03109999U (en) | 1990-02-26 | 1990-02-26 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03109999U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009530188A (en) * | 2006-03-21 | 2009-08-27 | ロッキード、マーティン、コーパレイシャン | Deployable articulated satellite with articulated thermal radiator and method of operating the satellite |
| WO2016097575A1 (en) * | 2014-12-17 | 2016-06-23 | Airbus Defence And Space Sas | Spacecraft |
-
1990
- 1990-02-26 JP JP1865990U patent/JPH03109999U/ja active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009530188A (en) * | 2006-03-21 | 2009-08-27 | ロッキード、マーティン、コーパレイシャン | Deployable articulated satellite with articulated thermal radiator and method of operating the satellite |
| WO2016097575A1 (en) * | 2014-12-17 | 2016-06-23 | Airbus Defence And Space Sas | Spacecraft |
| FR3030457A1 (en) * | 2014-12-17 | 2016-06-24 | Airbus Defence & Space Sas | SPACE ENGINE |
| US9828116B1 (en) | 2014-12-17 | 2017-11-28 | Airbus Defence And Space Sas | Spacecraft |