Sentinel 1

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Sentinel 1
Sentinel 1-IMG 5874-gradient.jpg
Operator ESA
Mission type Earth observation
Launch date 2013 (2013)
Launch vehicle Vega or Soyuz
Launch site Kourou, French Guiana
Mass ~2300 kg
Orbital elements
Regime Sun-synchronous dawn-dusk
Altitude 693 km
Orbital period ~96 minutes

Sentinel-1 is a future space mission from ESA of GMES program, consisting of a constellation of two satellites. The payload of Sentinel-1 is a Synthetic Aperture Radar in C-band which provides continuous imagery (day, night and all weather).

On 12 March 2010, the European Space Agency and Thales Alenia Space signed a contract worth €270 million to build the second satellite of the Sentinel-1 pair.

A launch date in 2013 is foreseen.

Contents

Mission characteristics [edit]

  • Role: Earth Observation
  • Launch date: 2013
  • Launch mass: ~2300 kg
  • Launcher: Vega or Soyuz
  • Launch location: Kourou, French Guiana
  • Orbit: Sun-synchronous dawn-dusk
  • Altitude: 693 km
  • Orbit cycle: ~96 minutes
  • Nominal duration: 7.25 years

Instruments [edit]

Sentinel-1 spacecraft are designed to carry a single C-band SAR, data storage capacity of 1,410 Gbit and 520 Mbit/s X-band downlink capacity.

Applications [edit]

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

A summary of applications are:

  • Monitoring sea ice zones and the Arctic environment, and surveillance of marine environment.
  • Monitoring land surface motion risks
  • Mapping of land surfaces: forest, water and soil
  • Mapping in support of humanitarian aid in crisis situations

Industrial [edit]

Prime contractor of mission is Thales Alenia Space Italy. SAR instrument will be the responsibility of Astrium Gmbh.

External links [edit]