Tuesday, October 2, 2001

ERS-1

 1991-050A


The European Space Agency's ERS-1 Earth Resources Satellite was launched on 1991 Jul 17 into a sun-synchronous orbit. Built by Dornier but based on Matra's SPOT Mk 1 bus, ERS 1 carried a 10-m x 1m SAR antenna used by the 5.3GHz Active Microwave Instrument, as well as altimeters and laser reflectors.

The orbit adjust engine restores the orbit when it drifts by 1 km, in a two-burn maneuver half an orbit apart. The burns are needed every 2 weeks at solar maximum, once a month otherwise, with inclination maneuvers every 9 to 10 months. 


ERS 1 
 

DateTimeEventOrbit  

1991 Jul 17  0146:31  Launch by Ariane 
  T+2:37 St 1 sep 
  T+2:40 St 2 MES 
  T+3:20 Fairing 02 sep
  T+4:46 St 2 sep 
  T+4:51 St 3 MES 
 0203:16 T+16:45 St 3 MECO 
 0204:14  T+17:43 ERS-1 sep 
 0205:54  T+19:23 ASAP payloads sep 
   100.44 776 x 782 x 98.52 
1991 Jul 20   TCM 
1991 Jul 26   TCM to `Venice orbit' 
1996 Aug   end of regular ops
1997 Jun 22  100.54 783 x 785 x 98.5 
1997 Jun 25  
TCM COLA 1 m/s to avoid K-614  100.58 784 x 788 x 98.6 
1997 Jun 26    100.54 783 x 785 x 98.5 
2000 Mar 10end of ops 

Payload:

  • AMI Active Microwave Instrument 5.3 GHz 10mx1m

    • SAR imager

    • SAR Wave mode

    • SAR Wind scatterometer

  • RA Radar Altimeter

  • ASTR Along Track Scanning Radiometer/Microwave sounder

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