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(Redirected from Spacecraft bus)
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/spacecraft, in which the payload and all scientific instruments are held.

Bus-derived satellites are less customized than specially-produced satellites, but have specific equipment added——to meet 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.

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."

Some satellite bus examples include:

Components

A bus typically consists of the following subsystems:

See also

References

  1. ^ "TU Delft: Spacecraft bus subsystems". Lr.tudelft.nl. Archived from the original on 2016-03-03. Retrieved 2014-04-23.
  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. Archived from the original on 2014-02-20. 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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