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Satellite bus

From Wikipedia, the free encyclopedia
Communications satellite bus and payload module

Asatellite bus(orspacecraft bus) is the main body and structural component of asatelliteorspacecraft,in which thepayloadand all scientific instruments are held.

Bus-derived satellites are less customized than specially-produced satellites, but have specific equipment added to meetcustomer requirements,for example with specializedsensorsortransponders,in order to achieve a specific mission.[1][2][3][4]

They are commonly used forgeosynchronoussatellites, particularlycommunications satellites,but are also used in spacecraft which occupy lower orbits, occasionally includinglow Earth orbitmissions.

Examples[edit]

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[edit]

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

See also[edit]

References[edit]

  1. ^"TU Delft: Spacecraft bus subsystems".Lr.tudelft.nl. Archived fromthe originalon 2016-03-03.Retrieved2014-04-23.
  2. ^"Spacecraft Systems".Braeunig.us.Retrieved2014-04-23.
  3. ^"The James Webb Space Telescope".Jwst.nasa.gov.Retrieved2014-04-23.
  4. ^"Antrix Corporation Ltd - Satellites > Spacecraft Systems & Sub Systems".Antrix.gov.in. 2009-09-24. Archived fromthe originalon 2014-02-20.Retrieved2014-04-23.
  5. ^"Status of the JWST Sunshield and Spacecraft"(PDF).
  6. ^Satellite Bus SubsystemsArchived2012-09-05 at theWayback Machine,NEC, accessed 25 August 2012.

External links[edit]