JPH0260261U - - Google Patents
Info
- Publication number
- JPH0260261U JPH0260261U JP14021688U JP14021688U JPH0260261U JP H0260261 U JPH0260261 U JP H0260261U JP 14021688 U JP14021688 U JP 14021688U JP 14021688 U JP14021688 U JP 14021688U JP H0260261 U JPH0260261 U JP H0260261U
- Authority
- JP
- Japan
- Prior art keywords
- solar
- solar cell
- spacecraft
- paddle
- 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
- 230000005855 radiation Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Description
第１図は、この考案の一実施例を示す太陽電池
パドルの構成図、第２図は従来の太陽電池パドル
の構成図、第３図は太陽電池パドルを展開した宇
宙機の軌道上太陽指向状態を示す図である。図に
おいて１は太陽電池、２は太陽電池１を貼付ける
パネル（あるいはシート）、３は太陽電池パドル
の反太陽指向面に施した低赤外放射率の熱制御材
、４は宇宙機内の発熱を宇宙空間へ排熱する放熱
面、５は宇宙機に照射する太陽光、６は宇宙機放
熱面に照射する太陽電池パドル反太陽指向面から
の赤外光である。なお、図中同一あるいは相当部
分には同一符号を付して示してある。
Figure 1 is a configuration diagram of a solar array paddle showing an embodiment of this invention, Figure 2 is a diagram of a conventional solar array paddle, and Figure 3 is a solar array pointing toward the sun in orbit of a spacecraft with the solar array paddle deployed. It is a figure showing a state. In the figure, 1 is a solar cell, 2 is a panel (or sheet) to which the solar cell 1 is attached, 3 is a heat control material with low infrared emissivity applied to the anti-solar surface of the solar array paddle, and 4 is heat generated inside the spacecraft. 5 is sunlight that irradiates the spacecraft, and 6 is infrared light from the anti-sun direction surface of the solar battery paddle that irradiates the spacecraft heat dissipation surface. It should be noted that the same or corresponding parts in the figures are indicated by the same reference numerals.
Claims (1)
陽光受光面側に太陽電池が貼付けられ、軌道上で
太陽光エネルギーを吸収し宇宙機に供給する電力
を発生する太陽電池パドルにおいて、太陽電池貼
付面と反対の面（反太陽指向面）に赤外放射率の
低いコーテイングを施し反太陽指向面からの赤外
放射量を少なくしたことを特徴とする太陽電池パ
ドル。 Solar cells are attached to the sunlight-receiving surface side of the solar cell attached panel (or sheet), and the solar cell paddle absorbs sunlight energy in orbit and generates power to be supplied to the spacecraft. A solar cell paddle characterized in that the opposite surface (anti-solar oriented surface) is coated with a low infrared emissivity to reduce the amount of infrared radiation from the anti-solar oriented surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14021688U JPH0260261U (en) | 1988-10-27 | 1988-10-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14021688U JPH0260261U (en) | 1988-10-27 | 1988-10-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0260261U true JPH0260261U (en) | 1990-05-02 |
Family
ID=31404187
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP14021688U Pending JPH0260261U (en) | 1988-10-27 | 1988-10-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0260261U (en) |
-
1988
- 1988-10-27 JP JP14021688U patent/JPH0260261U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2362286A1 (en) | Solar cell array orientation in an airship | |
| JP2016521225A (en) | Spacecraft, thermal control system and thermal control panel | |
| EP0896372A3 (en) | Solar battery module | |
| JPH0260261U (en) | ||
| WO1989002055A1 (en) | Solar energy conversion device | |
| JP3143010B2 (en) | Solar panel and roof of building using the same | |
| JP2973996B2 (en) | Spacecraft power recovery structure | |
| JPH03109999U (en) | ||
| JPH03127868A (en) | Solar battery power source device | |
| ORTABASI | A hardened solar concentrator system for space power generation-Photovoltaic cavity converter(PVCC) | |
| JPS61148799U (en) | ||
| JPS63167212U (en) | ||
| JPS6449594U (en) | ||
| JPS5991760U (en) | Failure detection device for solar array paddles | |
| JPS63143500U (en) | ||
| JPH042880Y2 (en) | ||
| JPS58188300U (en) | Solar panels on spin-stabilized satellites | |
| JPS6262600U (en) | ||
| AU613964B2 (en) | Solar energy conversion device | |
| JPS6350146U (en) | ||
| JPS61168652U (en) | ||
| JPH10258800A (en) | Solar cell panel and satellite using it | |
| JP2001041591A (en) | Photothermal material high efficiency energy apparatus | |
| Cong | Anodized aluminum and aluminum alloy coatings for thermal control | |
| Zakhidov | Modeling solar energy concentrators. |