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Satellite bus

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

Examples
Some satellite bus examples include: • Boeing DS&S 702Lockheed Martin Space Systems A2100Moog Inc. SL-OMV, Meteor, Meteorite • • INVAP ARSAT-3KAirbus D&S EurostarISRO's I-1K, I-2K, I-3K, I-4K, I-6K, and Indian Mini Satellite busNASA Ames MCSBSSL 1300 • family • Orbital ATK Star Bus family, inc GEOStarMitsubishi Electric DS2000Spacecraft bus of the James Webb Space TelescopeSPUTNIX TabletSatSPUTNIX OrbiCraft-Pro ==Components==
Components
A bus typically consists of the following subsystems: • Command and data handling (C&DH) system • Communications system and antennas • Electrical power system (EPS) • PropulsionThermal controlAttitude control system (ACS) • Guidance, navigation, and control (GNC) system • Structures and trussesLife support (for crewed missions). ==See also==
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