Sentinel-1

Sentinel-1 is the first of the Copernicus Programme satellite constellation conducted by the European Space Agency.[4] This mission is composed of a constellation of two satellites, Sentinel-1A and Sentinel-1B, which share the same orbital plane. They carry a C-band synthetic-aperture radar instrument which provides a collection of data in all-weather, day or night. This instrument has a spatial resolution of down to 5 m and a swath of up to 400 km. The constellation is on a sun synchronous, near-polar (98.18°) orbit. The orbit has a 12-day repeat cycle and completes 175 orbits per cycle.

Sentinel-1
Model of a Sentinel 1 (radar antenna missing)
Manufacturer
OperatorEuropean Space Agency
ApplicationsLand and sea monitoring, natural disasters mapping, sea ice observations, ships detection
Specifications
Spacecraft typeSatellite
ConstellationActive: 2 (4 planned)
Design life7 years
Launch mass2,300 kg (5,100 lb)
Dry mass2,170 kg (4,780 lb)
Dimensions3.9 m × 2.6 m × 2.5 m (13 ft × 8.5 ft × 8.2 ft)
Power5.9 kilowatts (5,900 W)[2]
Batteries324 Ah
Production
StatusActive
Built2
On order2
Launched2
Operational2
Maiden launchSentinel-1A (3 April 2014)[3]
Last launchSentinel-1D (TBD)
Related spacecraft
Subsatellite ofCopernicus Programme
Sentinel-2

The first satellite, Sentinel-1A, launched on 3 April 2014, and Sentinel-1B was launched on 25 April 2016. Both satellites lifted off from the same location in Kourou, French Guiana, and each on a Soyuz rocket.[5] Sentinel-1C and 1D are in development with launch dates to be determined.

There are a wide range of applications for the data collected via the Sentinel-1 mission. A few of these uses include sea and land monitoring, emergency response due to environmental disasters, and economic applications. A major goal of the mission was to provide C-Band SAR data.[6]Recently, Sentinel-1 has worked in conjunction with SMAP (Soil Moisture Active and Passive) to help achieve a more accurate measure of soil moisture estimates.[7] Observations from both instruments show to be complementary of each other as they combine data of soil moisture contents.

The ESA and European Commission's policies makes Sentinel-1's data easily accessible. Various users can acquire the data and use it for public, scientific, or commercial purposes for free.

Instruments

Sentinel-1 spacecraft are designed to carry the following instruments:[8]

  • A single C-band synthetic-aperture radar (C-SAR) with its electronics. This instrument provides 1 dB radiometric accuracy with a central frequency at 5.405 GHz.[9] The data collected in C-SAR was made to be continuous after the termination of a previous mission (Envisat mission).[10]
  • An SDRAM-based Data Storage and Handling Assembly (DSHA), with an active data storage capacity of about 1,443 Gbit (168 GiB), receiving data streams from SAR-SES over two independent links gathering SAR_H and SAR_V polarization, with a variable data rate up to 640 Mbit/s on each link, and providing 520 Mbit/s X-band fixed-user data-downlink capability over two independent channels towards ground.

Characteristics

Specifications of the Sentinel-1 satellites:[9]

  • 7 year lifetime (12 years for consumables)
  • Launcher: Soyuz
  • Near-polar (98.18°) Sun-synchronous orbit
  • 693 km (431 mi) altitude
  • 12-day repeat cycle
  • 175 revolutions per cycle
  • 98.6 minute orbital period
  • 3-axis altitude stabilization
  • 2,300 kg (5,100 lb) launch mass
  • 3.9 m × 2.6 m × 2.5 m (12.8 ft × 8.5 ft × 8.2 ft) dimensions

Operational/acquisition modes

Sentinel-1 has four operational modes:[9][11][12]

  • Strip Map (SM) Mode features 5-by-5-metre (16 by 16 ft) spatial resolution and an 80 km (50 mi) swath.
    • The sole uses of SM are to monitor small islands as well as emergency management for extraordinary events upon request
    • Offers data products in single (HH or VV) or double (HH + HV or VV + VH) polarization
  • Interferometric Wide Swath (IW) Mode features 5-by-20-metre (16 by 66 ft) spatial resolution and a 250 km (160 mi) swath.
    • IW is the main operational mode over land
    • IW accomplishes interferometry through burst synchronization
    • Offers data products in single (HH or VV) or double (HH + HV or VV + VH) polarization
  • Extra Wide Swath (EW) Mode features 25-by-100-metre (82 by 328 ft) spatial resolution and a 400 km (250 mi) swath.
    • EW is used mainly to monitor wide coastal areas for phenomena such as shipping traffic and potential environmental hazards like oil spills or changes in sea ice.
    • Offers data products in single (HH or VV) or double (HH + HV or VV + VH) polarization
  • Wave (WV) Mode features 5-by-20-metre (16 by 66 ft) resolution and a low data rate. It produces 20 by 20 km (12 by 12 mi) sample images along the orbit at intervals of 100 km (62 mi).[9]
    • This is the main operational mode over open ocean.
    • Offers data products only in single (HH or VV) polarization

Data products

Sentinel-1 has four types of data products:[11]

  • Raw Level 0 data
  • Processed Level 1 Single Look Complex (SLC) data:
    • Complex images with phase and amplitude of specified areas
  • Ground Range Detected (GRD) Level 1 data:
    • Only systematically distributed multi-looked intensity
  • Level 2 Ocean (OCN) data:
    • Systematically distributed data of ocean's geophysical parameters

All data levels are publicly available for free online within 24 hours of observation.[13]

Applications

Sentinel-1 will provide continuity of data from the ERS and Envisat missions, with further enhancements in terms of revisit, coverage, timeliness and reliability of service.

A summary of the main applications of Sentinel-1 include:[14]

  • Marine monitoring
    • Sea-ice levels and conditions
    • Ocean oil spills
    • Ship activity
    • Marine winds
  • Land monitoring
    • Agriculture
    • Forestry
    • Subsidence
      • The C-SAR instrument is capable of measuring land subsidence through the creation of interferometric synthetic-aperture radar (InSAR) images. The analysis of phase changes between two or more synthetic aperture radar images taken at different times is able to create maps of the digital elevation and measure the land surface deformation of an area. High spatial (20m) and temporal (6 days) resolutions allow S1 to improve on current InSAR techniques and provide systematic continuity to the data.[15]
  • Emergency response
    • Flooding
    • Landslide and volcanic
    • Earthquakes

Industrial

The prime contractor of the mission is Thales Alenia Space Italy, with whole system integration and also with production of platform Spacecraft Management Unit (SMU) and payload Data Storage and Handling Assembly (DSHA). Sentinel-1A was constructed in Rome, Italy. Other technologies such as the T/R modules, the C-band synthetic-aperture radar antenna, the advanced data management and transmission subsystems, and the on-board computer, were developed in L'Aquila and Milan.[17] The C-SAR instrument is the responsibility of Astrium Gmbh.

The ground segment prime contractor is Astrium with subcontractors Telespazio, WERUM, Advanced Computer Systems and Aresys. Final test verification of the satellite was completed at Thales Alenia Space's clean rooms in Rome and Cannes.[17]

Spacecraft

  • Sentinel-1A – launched on 3 April 2014[3]
  • Sentinel-1B – launched on 25 April 2016[3]
  • Sentinel-1C – development contract signed with Thales Alenia Space of Italy in December 2015, launch date TBD[18]
  • Sentinel-1D – development contract signed with Thales Alenia Space of Italy in December 2015, launch date TBD[18]

Examples of images produced from Sentinel-1 data.

References

  1. "Sentinel 1". Earth Online. European Space Agency. Retrieved 17 August 2014.
  2. "Sentinel 1 Datasheet" (PDF). ESA. August 2013. Retrieved 17 August 2014.
  3. "Earth Online – Sentinel 1". European Space Agency. Retrieved 3 April 2014.
  4. "Sentinel-1". Sentinel Online. European Space Agency. Retrieved 21 March 2018.
  5. "Soyuz overview". Arianespace. Retrieved 21 March 2018.
  6. "Sentinel-1 - ESA EO Missions - Earth Online - ESA". earth.esa.int. Retrieved 2020-03-05.
  7. Lievens, H.; Reichle, R. H.; Liu, Q.; De Lannoy, G. J. M.; Dunbar, R. S.; Kim, S. B.; Das, N. N.; Cosh, M.; Walker, J. P. (2017-06-27). "Joint Sentinel-1 and SMAP data assimilation to improve soil moisture estimates". Geophysical Research Letters. 44 (12): 6145–6153. Bibcode:2017GeoRL..44.6145L. doi:10.1002/2017gl073904. ISSN 0094-8276. PMC 5896568. PMID 29657343.
  8. "Sentinel-1: Instrument Payload". Sentinel Online. European Space Agency. Retrieved 7 March 2017.
  9. Attema, Evert; et al. (August 2007). "Sentinel-1: The Radar Mission for GMES Operational Land and Sea Services" (PDF). Bulletin. 131: 10–17. Bibcode:2007ESABu.131...10A.
  10. "Sentinel-1 - ESA EO Missions - Earth Online - ESA". earth.esa.int. Retrieved 2020-03-05.
  11. "User Guides - Sentinel-1 SAR - Acquisition Modes". Sentinel Online. European Space Agency. Retrieved 12 March 2018.
  12. "Sentinel 1 Data Access and Products". European Space Agency. March 2015. Retrieved 11 March 2018.
  13. "Sentinel-1 - Data Distribution Schedule - Missions - Sentinel Online". sentinel.esa.int. Retrieved 2020-03-05.
  14. "User Guides - Sentinel-1 SAR - Applications". Sentinel Online. European Space Agency. Retrieved 22 March 2018.
  15. Cian, Fabio; Blasco, José Manuel Delgado; Carrera, Lorenzo (March 2019). "Sentinel-1 for Monitoring Land Subsidence of Coastal Cities in Africa Using PSInSAR: A Methodology Based on the Integration of SNAP and StaMPS". Geosciences. 9 (3): 124. doi:10.3390/geosciences9030124.
  16. Amos, Jonathan (2 September 2014). "Sentinel system pictures Napa quake". BBC News. Retrieved 2 September 2014.
  17. "Sentinel-1A Arrives at Launch Site in French Guiana". Thales Group. 24 February 2014. Retrieved 15 March 2018.
  18. "Decolla la space economy italiana" [Take off of the Italian space economy] (in Italian). Airpress. 2015-12-15. Retrieved 15 December 2015.
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