Satellite bus

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Communications satellite bus and payload module

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.[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[]

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[]

  1. ^ "TU Delft: Spacecraft bus subsystems". Lr.tudelft.nl. Retrieved 2014-04-23.{{cite web}}: CS1 maint: url-status (link)
  2. ^ "Spacecraft Systems". Braeunig.us. Retrieved 2014-04-23.
  3. ^ "The James Webb Space Telescope". Jwst.nasa.gov. Retrieved 2014-04-23.
  4. ^ "Antrix Corporation Ltd - Satellites > Spacecraft Systems & Sub Systems". Antrix.gov.in. 2009-09-24. Retrieved 2014-04-23.
  5. ^ "Status of the JWST Sunshield and Spacecraft" (PDF).
  6. ^ Satellite Bus Subsystems Archived 2012-09-05 at the Wayback Machine, NEC, accessed 25 August 2012.

External links[]

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