JPS58149300U - Artificial satellite - Google Patents

Artificial satellite

Info

Publication number
JPS58149300U
JPS58149300U JP4710782U JP4710782U JPS58149300U JP S58149300 U JPS58149300 U JP S58149300U JP 4710782 U JP4710782 U JP 4710782U JP 4710782 U JP4710782 U JP 4710782U JP S58149300 U JPS58149300 U JP S58149300U
Authority
JP
Japan
Prior art keywords
satellite
power generating
generating body
balloon
solar cells
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
Application number
JP4710782U
Other languages
Japanese (ja)
Inventor
健一 稲宮
Original Assignee
三菱電機株式会社
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 三菱電機株式会社 filed Critical 三菱電機株式会社
Priority to JP4710782U priority Critical patent/JPS58149300U/en
Publication of JPS58149300U publication Critical patent/JPS58149300U/en
Pending legal-status Critical Current

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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

【図面の簡単な説明】[Brief explanation of drawings]

第1図は一般的な三軸制御型衛星の構成図である。第2
図はこの考案に係る人工衛星の構成−である。 図中、′1は衛星本体、3は太陽電池、4は風船状の発
電体、5は可とう棒、6はケーブルである。 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 configuration diagram of a typical three-axis controlled satellite. Second
The figure shows the configuration of the artificial satellite according to this invention. In the figure, '1 is the satellite body, 3 is a solar cell, 4 is a balloon-shaped power generating body, 5 is a flexible rod, and 6 is a cable. Note that the same or corresponding parts in the figures are indicated by the same reference numerals.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 表面に複数の太陽電池が取付けられ、かつ所定の軌道投
入時又軌道上においてその中空部に気体を封入すること
により膨張する風船状の発電体と、衛星本体と上記風船
状の発電体とを電気的に接続し、発電体の太陽電池で発
生する電力を衛星本体に送電するためのケーブルと、上
記衛星本体と上記発電体とを結合し、上記衛星本体の制
御系の時−定数から上記発電体の時定数を分離でき、か
つ上記発電体に受けた外乱によって発生する振動エネル
ギーを摩擦により吸収する可とう性の棒材とを備えた人
工衛星。
A balloon-shaped power generating body has a plurality of solar cells attached to its surface and expands by filling a hollow space with gas when entering a predetermined orbit or while on orbit, and a satellite body and the balloon-shaped power generating body. A cable for electrically connecting and transmitting the electric power generated by the solar cells of the power generation body to the satellite body is connected to the satellite body and the power generation body, and the above is calculated from the time-constant of the control system of the satellite body. An artificial satellite comprising a flexible bar that can separate the time constant of a power generating body and absorbs vibrational energy generated by disturbances received by the power generating body through friction.
JP4710782U 1982-04-01 1982-04-01 Artificial satellite Pending JPS58149300U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4710782U JPS58149300U (en) 1982-04-01 1982-04-01 Artificial satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4710782U JPS58149300U (en) 1982-04-01 1982-04-01 Artificial satellite

Publications (1)

Publication Number Publication Date
JPS58149300U true JPS58149300U (en) 1983-10-06

Family

ID=30058078

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4710782U Pending JPS58149300U (en) 1982-04-01 1982-04-01 Artificial satellite

Country Status (1)

Country Link
JP (1) JPS58149300U (en)

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