Sentinel-5 Precursor

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Sentinel-5 Precursor
Sentinel 5P model.jpg
Sentinel-5P model
Manufacturer
Operator ESA
Applications Atmospheric composition, air pollution, ozone layer monitoring
Specifications
Spacecraft type Satellite
Bus Astrobus-L 250 M[1]
Design life 7 years
Launch mass 900 kilograms (2,000 lb)
Dry mass 820 kilograms (1,810 lb)
Dimensions Lua error in Module:Convert at line 1851: attempt to index local 'en_value' (a nil value). - height × width × length[2]
Power 1,500 watts (2.0 hp)
Batteries 156 Ah
Equipment TROPOMI
Production
Status Under construction
Built 0
On order 1
Launched 0
Operational 0
Maiden launch 2016[3]
Related spacecraft
Subsatellite of Sentinel constellation
← Sentinel-4 Sentinel-5 →

Sentinel-5 Precursor (Sentinel-5P) is an Earth observation satellite developed by the ESA as part of the Copernicus Programme to close the gap in continuity of observations between Envisat and Sentinel-5.[4]

Overview

Sentinel-5 Precursor will be the first mission of a Copernicus Programme dedicated to monitoring air pollution. It's instrument will be ultraviolet, visible, near and short-wavelength infrared spectrometer called Tropomi. Satellite is build on a hexagonal Astrobus L 250 satellite bus equipped in S- and X-band communication antennas, three foldable solar panels generating 1500W and a hydrazine thrusters for station-keeping.[1][2]

Once launched satellite will be put on 824 km Sun-synchronous orbit with a period of 13:30 hours.

Tropomi

Tropomi (TROPOspheric Monitoring Instrument) will be a spectrometer sensing ultraviolet (UV), visible (VIS), near (NIR) and short-wavelength infrared (SWIR) to monitor ozone, methane, formaldehyde, aerosol, carbon monoxide, NO2 and SO2 in the atmosphere extending the capabilities of OMI from Aura satellite and SCIAMACHY instrument from Envisat.[5]

Instrument will be taking measurements every second covering an area of approximately 2600km wide and 7km long in a resolution of 7x7km. Light will be separated into a different wavelengths using grating spectrometers and then measured with four different detectors for respective spectral bands. UV spectrometer is going to work in spectral range of 270-320nm, visible light spectrometer in 310-500nm, NIR in 675-775nm and SWIR in 2305-2385nm.[6]

Instrument is split into four major blocks: UV-VIS-NIR spectrometers and a calibration block, SWIR spectrometer with its optics, instrument control unit and a cooling block. Total mass of Tropomi will be 200kg with a power consumption of 170W on average and a data output of 140 Gbits per orbit.[6][1]

Instrument is being build by a joint venture between the Netherlands Space Office, Royal Netherlands Meteorological Institute, Netherlands Institute for Space Research, Netherlands Organisation for Applied Scientific Research and Airbus Defence and Space Netherlands.[7][8]

The SWIR spectrometer was designed and built by the Optical Payloads Group of Surrey Satellites (SSTL); it employs an immersed grating design in which light impinges upon an etched grating from within a high-index substrate (silicon in this case). The reduced wavelength within the refractive medium permits an efficient, space-saving design. The SWIR grating was provided by SRON (Netherlands), who also provided the Front-End Electronics (FEE). The SWIR spectrometer receives light from the main instrument via an intermediate pupil, and directs this - via a telescope - towards a slit which defines the along-track footprint of the instrument on the ground. Light from the slit is re-collimated, diffracted by the immersed-grating at high-order and finally imaged onto a two-dimensional detector by a high aperture relay lens. The SWIR detector (furnished by Sofradir, France) has 256 elements in the across-track direction and 1024 elements in the spectral direction (the element pitch is 30 microns); it is operated cold (typically 140 K). The SWIR spectrometer optics are mounted on a cooled optical bench (approximately 200K) and the instrument is insulated by a multiple-layer insulation (MLI) blanket. The SWIR instrument was aligned, focussed and characterised at the Mullard Space Science laboratory thermal vacuum facility in Surrey, UK.

History

First large contract for Sentinel-5P was signed in July 2009 for Tropomi instrument between the European Space Agency and Dutch Ministry of Economic Affairs which contributed €78 million.[7] On 8 December 2011 ESA selected Astrium UK as a prime contractor for the satellite, signing contract worth €45.5 million[9] Construction of the satellite itself was completed in May 2014, however it still awaits for its primary instrument.[10]

Satellite will be launched by Eurockot Launch Services onboard Rokot in 2016.[3]

References

  1. ↑ 1.0 1.1 1.2 Lua error in package.lua at line 80: module 'strict' not found.
  2. ↑ 2.0 2.1 Lua error in package.lua at line 80: module 'strict' not found.
  3. ↑ 3.0 3.1 Lua error in package.lua at line 80: module 'strict' not found.
  4. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  5. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  6. ↑ 6.0 6.1 Lua error in package.lua at line 80: module 'strict' not found.
  7. ↑ 7.0 7.1 Lua error in package.lua at line 80: module 'strict' not found.
  8. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  9. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  10. ↑ Lua error in package.lua at line 80: module 'strict' not found.

External links

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