JPS6237600U - - Google Patents
Info
- Publication number
- JPS6237600U JPS6237600U JP13021685U JP13021685U JPS6237600U JP S6237600 U JPS6237600 U JP S6237600U JP 13021685 U JP13021685 U JP 13021685U JP 13021685 U JP13021685 U JP 13021685U JP S6237600 U JPS6237600 U JP S6237600U
- Authority
- JP
- Japan
- Prior art keywords
- satellite
- spin
- north
- around
- artificial satellite
- 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
- Details Of Aerials (AREA)
Description
第１図はこの考案の一実施例を示す静止スピン
型人工衛星の説明図、第２図は従来の静止スピン
型人工衛星を示す説明図である。
図において、１は人工衛星本体、２は太陽電池
パネル、３はアンテナ、４はスピン軸、５ａ，５
ｂ，５ｃは太陽光到来方向、６は太陽光遮蔽体を
示す。なお、図中同一符号は同一または相当部分
を示す。
FIG. 1 is an explanatory diagram of a geosynchronous spin type artificial satellite showing one embodiment of this invention, and FIG. 2 is an explanatory diagram of a conventional geosynchronous spin type artificial satellite. In the figure, 1 is the satellite body, 2 is the solar panel, 3 is the antenna, 4 is the spin axis, 5a, 5
b and 5c indicate the direction of arrival of sunlight, and 6 indicates a sunlight shielding body. Note that the same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
に衛星本体が回転し、地球指向をミツシヨンとす
る静止スピン安定型人工衛星において、人工衛星
本体の南北面のまわりに太陽光遮蔽体を備えたこ
とを特徴とする静止スピン安定型人工衛星。 A geostationary spin-stabilized artificial satellite that has a spin axis in the north-south direction, around which the satellite body rotates, and whose mission is to point toward the earth.A satellite that is equipped with solar shields around the north-south faces of the satellite body. A geosynchronous spin-stabilized artificial satellite characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13021685U JPS6237600U (en) | 1985-08-27 | 1985-08-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13021685U JPS6237600U (en) | 1985-08-27 | 1985-08-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6237600U true JPS6237600U (en) | 1987-03-05 |
Family
ID=31027499
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13021685U Pending JPS6237600U (en) | 1985-08-27 | 1985-08-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6237600U (en) |
-
1985
- 1985-08-27 JP JP13021685U patent/JPS6237600U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE3278633D1 (en) | Communication satellite system in geostationary loop positions | |
| GB1400850A (en) | Communication system using geosynchronous satellites in quasiequatorial orbits | |
| GB1201547A (en) | Communications satellite | |
| AU527284B2 (en) | Welded spherical valve body | |
| JPS54126092A (en) | Superconductive solenoid with axis inclination correcting function | |
| JPS6237600U (en) | ||
| GR3000547T3 (en) | Shading device for use in a geostatic satellite | |
| JPS61157100U (en) | ||
| JPS6226300U (en) | ||
| JPS60170299U (en) | Geostationary three-axis stable satellite | |
| JPS59139499U (en) | three axis satellite | |
| JPS60191600U (en) | solar irradiation device | |
| JPH0359299U (en) | ||
| RUDOLF et al. | Star field attitude sensor study for the Pioneer Venus spacecraft(Characteristics of star field attitude sensor for installation in Pioneer Venus spacecraft) | |
| Williams et al. | Design considerations for an amateur solar sail spacecraft | |
| JPS5991018U (en) | geostationary communication satellite | |
| BUEDELER | Repair in outer space | |
| JPS59196399U (en) | Satellite attitude control device | |
| MULLEN et al. | High-level spacecraft charging environments near geosynchronous orbit[Interim Scientific Report] | |
| JPH0444674U (en) | ||
| HILLARD | Control of a synchronous satellite with large flexible arrays using a double gimbaled momentum wheel(solar arrays)[Ph. D. Thesis] | |
| SCHEIL | Design criteria and state of development of the HEOS-A satellite(Highly eccentric orbit satellite/HEOS/ for solar wind, cosmic ray and magnetic field data collection, noting design and mission program) | |
| JPH01128496U (en) | ||
| BERNUSSOU | Contribution of the study of nonlinear recurrence solutions: Application to the study of certain modulation systems[Ph. D. Thesis] | |
| WAGNER et al. | Orbit targeting for body stabilized synchronous satellites with attitude constraints |