ERS overview


 
 
MARISS service
 
MARISS service
 
 
 
3D visualisation of InSAR derived elevation data on Baffin Islan
 
3D visualisation of InSAR derived elevation data on Baffin Island
 
 
 
The Strait of Messina, Italy
 
ERS-2 radar view of Strait of Messina, Italy
 
 
 
ERS-2 composite highlighting tsunami damage
 
ERS-2 composite highlighting tsunami damage
 
 
 
Greenland
 
Seasonal results from the survey
 
 
 
ERS-2
 
ERS-2 satellite and applications
 
 
The European Remote Sensing satellite ERS-1, launched in 1991, carried a comprehensive payload including an imaging synthetic aperture radar, a radar altimeter and other powerful instruments to measure ocean surface temperature and winds at sea. ERS-2, which overlapped with ERS-1, was launched in 1995 with an additional sensor for atmospheric ozone research.

At their time of launch the two ERS satellites were the most sophisticated Earth observation spacecraft ever developed and launched by Europe. These highly successful ESA satellites collected a wealth of valuable data on Earth’s land surfaces, oceans, and polar caps and were called upon to monitor natural disasters such as severe flooding or earthquakes in remote parts of the world.

Both ERS satellites were built with a core payload of two specialised radars and an infrared imaging sensor. The two were designed as identical twins with one important difference: ERS-2 included an extra instrument to monitor ozone levels in the atmosphere.

Shortly after the launch of ERS-2 in 1995 ESA decided to link the two satellites in the first ‘tandem’ mission which lasted for nine months. During this time the increased frequency and level of data available to scientists offered a unique opportunity to observe changes over a very short space of time, as both satellites orbited Earth only 24 hours apart.

In March 2000, a computer and gyro control failure led to ERS-1 finally ending its operations, after far exceeding its planned lifetime.

In July 2011, ERS-2 was retired and the process of deorbiting the satellite began.
 
 
  ERS - 1ERS - 2
Launchfrom Kourou,
French Guiana
17 July 199121 April 1995
LauncherAriane 4  
Launch mass 2384 kg2516 kg
Number of instruments4/5 including SAR
with GOME added to ERS-2
  
OrbitSun synchronous,
altitude 800 km
  
Inclination98.5 degrees  
Time for one orbit100 minutes  
Cycle35-day repeat  
 
 
 
Last update: 17 August 2011


In depth

 •  ERS technical site (http://earth.esa.int/ers/)