Satellite bus explained

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 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.[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

See main article: Comparison of satellite buses. Some satellite bus examples include:

Components

See main article: article. A bus typically consists of the following subsystems:[5]

See also

External links

Notes and References

  1. Web site: TU Delft: Spacecraft bus subsystems . dead . 2014-04-23 . Lr.tudelft.nl . 2016-03-03 . https://web.archive.org/web/20160303183439/http://www.lr.tudelft.nl/en/organisation/departments/space-engineering/space-systems-engineering/expertise-areas/spacecraft-engineering/design-and-analysis/configuration-design/subsystems/subsystems/ .
  2. Web site: Spacecraft Systems . Braeunig.us . 2014-04-23.
  3. Web site: The James Webb Space Telescope . Jwst.nasa.gov . 2014-04-23.
  4. Web site: Antrix Corporation Ltd - Satellites > Spacecraft Systems & Sub Systems . Antrix.gov.in . 2009-09-24 . 2014-04-23 . 2014-02-20 . https://web.archive.org/web/20140220164322/http://www.antrix.gov.in/sss_systems.html . dead .
  5. http://www.nec.com/en/global/solutions/space/satellite_bus/index.html Satellite Bus Subsystems