JPS60146000U

JPS60146000U - Artificial satellite

Info

Publication number: JPS60146000U
Application number: JP3365184U
Authority: JP
Inventors: 柳沢　祥雅
Original assignee: 三菱電機株式会社
Priority date: 1984-03-09
Filing date: 1984-03-09
Publication date: 1985-09-27

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

[Brief explanation of the drawing]

第１図は従来の人工衛星の図、第２図６１従来の人工衛
星での打上げ時の形状を示す図、第３図は従来の人工衛
星の内部を示す部分図、第４図は本考案の一実施例の人
工衛星の図、第５図は本考案の一実施例の人工衛星での
打上げ時の形状を示す図、第６図は第４図の内部を示す
部分図である。図中、”１は人工衛星本体、２は南北面構造壁、　　゛
　−３は東西面構造壁、４は地球指向壁、５は太陽型。池アレイ、６は機器、７は機器搭載板、８はヒートパイ
プ、９は放熱板、１０は蝶番、１１は可撓部分、１２は
機器である。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である。Figure 1 is a diagram of a conventional artificial satellite, Figure 2 is a diagram showing the shape of a conventional artificial satellite at the time of launch, Figure 3 is a partial diagram showing the inside of a conventional artificial satellite, and Figure 4 is a diagram of the present invention. FIG. 5 is a diagram showing the shape of an artificial satellite according to an embodiment of the present invention when it is launched, and FIG. 6 is a partial view showing the inside of FIG. 4. In the figure, 1 is the satellite body, 2 is the north-south structural wall, -3 is the east-west structural wall, 4 is the earth-oriented wall, 5 is the solar type, pond array, 6 is the equipment, 7 is the equipment mounting board, 8 is a heat pipe, 9 is a heat sink, 10 is a hinge, 11 is a flexible portion, and 12 is a device. In the drawings, the same or corresponding parts are denoted by the same reference numerals.

Claims

[Scope of utility model registration request]

An artificial satellite with geostationary three-axis attitude control, characterized in that a deployable heat sink and an equipment mounting section inside the satellite are thermally connected by a visible heat pipe.