Engineering:Satellite bus

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Short description: Main body and structural component of the satellite
Communications satellite bus and payload module

A satellite bus (or spacecraft bus) is the main body and structural component of a satellite or spacecraft, in which the payload and all scientific instruments are held.

Bus-derived satellites are different 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.[1][2][3][4]

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.

Examples

Main page: Astronomy:Comparison of satellite buses
Diagram of the James Webb Space Telescope's spacecraft bus. The solar panel is in green and the light purple flats are radiator shades.[5]

Some satellite bus examples include:

Components

A bus typically consists of the following subsystems:[6]

See also

References

External links

es:Satélite artificial#Modelo de satélite