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Sentinel-5 Precursor

Spacecraft and Launch Vehicles

Sentinel-5 Precursor, usually called Sentinel-5P, is a European Earth observation satellite developed by the European Space Agency for the Copernicus Programme. It was launched in October 2017 on a Rokot rocket from Plesetsk and was designed for a seven year life, bridging the gap in observations between Envisat and the later Sentinel-5 instruments. ESA selected Astrium UK, now part of Airbus Defence and Space, as prime contractor for the satellite in December 2011. The spacecraft is built on a hexagonal Astrobus L 250 satellite bus and carries a single instrument, the TROPOspheric Monitoring Instrument, which measures ozone, methane, formaldehyde, aerosol, carbon monoxide, nitrogen dioxide and sulphur dioxide in the atmosphere.

Facts
Year
2017 1
Propulsion
Hydrazine 2
Comparison
Body Style
Spacecraft 1
Connections

Exemplifies

Space Transport, Modes
Source Sentinel-5 Precursor (Wikipedia)

Of Make

Source Sentinel-5 Precursor (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Sentinel-5 Precursor (Wikipedia)Pre-launch
Quote, Pre-launch
ESA selected Astrium UK as a prime contractor for the satellite

Originated In

Also in Geography Atlas: where this subject originated.

Source European Space Agency: Sentinel-5P satelliteSatellite platform
Quote, Satellite platform
The design of the satellite platform, which was led by Airbus Defence and Space in Stevenage, UK, is based on the Astrobus M.
Sources
1. Sentinel-5 Precursor (Wikipedia)
  • Lead, mission type
    is an Earth observation satellite developed by ESA
  • Launch
    was launched on 13 October 2017 at 09:27 UTC from Plesetsk Cosmodrome Site 133
  • Pre-launch
    ESA selected Astrium UK as a prime contractor for the satellite
View the Source
2. European Space Agency: Sentinel-5P satellite
European Space AgencySatellite platform, propulsion
Quote, Satellite platform, propulsion
The propulsion system, which is a monopropellant hydrazine system, has a capacity of 82 kg with four 1 N thrusters in two redundant pairs.
View the Source
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