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Spacecraft bus : ウィキペディア英語版 | Satellite bus
A satellite bus or spacecraft bus is the general model on which multiple-production satellite spacecraft are often based. The bus is the infrastructure of a spacecraft, usually providing locations for the payload (typically space experiments or instruments). They are commonly used for geosynchronous satellites, particularly communications satellites, but are also used in spacecraft which occupy lower orbits, occasionally including low Earth orbit missions. A bus-derived satellite would be used as opposed to a one-off, or specially produced satellite, such as Prospero X-3. Bus-derived satellites are usually customized to customer requirements, for example with specialized sensors or transponders, in order to achieve a specific mission. == Examples == (詳細はBoeing 702 * Astrium's Eurostar * Lockheed Martin Space Systems A2100 * Modular Common Spacecraft Bus * SSL 1300 * STAR Bus * * ISRO's I-1K, I-2K, I-3K, I-4K, and Indian Mini Satellite bus
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Satellite bus」の詳細全文を読む
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