A satellite bus (or spacecraft bus) is the main body and structural component of the satellite in which the payload and all scientific instruments and are held.
Bus-derived satellites are opposed to specially produced satellites. Bus-derived satellites are usually customized to customer requirements, for example with specialized sensors or transponders, in order to achieve a specific mission.
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.
Main article: Comparison of satellite buses
Some satellite bus examples include:
Main article: Spacecraft § Subsystems
A bus typically consists of the following subsystems:
((cite web)): CS1 maint: url-status (link)