Envisat 1

ESA


Spacecraft nº:

ESA spacecraft nº: 48


Launch data:

Designation 27386 / 02009A
Launch date 01 Mar 2002 - 01:07:59 UT
Launch site Kourou, ELA-3
Launch vehicle Ariane-5G (V145 / S/N511)
Mission Government: Remote sensing (to replace ERS)
Sun-synchronous LEO orbit:
Perigee/Apogee 784 x 790
Eccentricity 4,19E-04
Inclination 98.5°
Period 100.6 min

The cost is covered at 24.5% by France, 18.5% by the UK and 17.5 % by . The total program cost (satellite, launch and exploitation) is EUR 2.3 billion. Operated by ESA

Launched in the same orbit at ERS 2, separated by 30 minutes.

Specifications:


Prime contractor European Space Agency (ESA)
Platform Spot-Mk2
Operator ESA
Mass at launch 8211 kg
Mass in orbit  
Payload mass 2050 kg
Fuel mass 319 kg
Dimension 26 m x 10 m x 5 m
Solar array 14 m (weighs 400 kg)
Stabilization  
DC power EOL: 6500 W
Design lifetime 5 years

End of live:

End of Operation:  08 April 2012
Cause:  

2 on-board recorders provide 70 Gbits each storage and a backup tape storage is available too. Inter orbit link in Ka-band will be possible with Artemis (another ESA satellite which could be launched in 1999 via H2). The service module is largely derived from Spot 4.

X-band science data downlink upto 2 x 100 Mbps
S-band command and control: 2 kpbs uplink, 4 kbps downlink

10 scientific payloads:

  • ASAR (Advanced Synthetic Aperture Radar): radar imaging, C-band, 27 m resolution. Built by Astrium
  • GOMOS (Global Ozone Monitoring by Occultation of Stars)
  • AATSR (Advanced Along Track Scanning Radiometer): IR radiometer
  • MWR (MicroWave Radiometer)
  • MERIS (Medium Resolution Imaging Spectrometer): visible and near IR imaging. Built by Alcatel Space
  • MIPAS (Michelson Interferometer for Passive Atmospheric Sounding)
  • SCIAMACHY (Scanning Imaging Absorption Spectrometer for Atmospheric Cartography)
  • RA-2 (Radar Altimeter)
  • DORIS (Doppler Orbitography and Radiopositioning Integrated by Satellite): orbitography
  • LRR (Laser Retro-Reflector)
  • The French Scarab experiment was withdrawn


Many of these instruments were on ERS satellites and will followup.


Assembling:

The launch campaign for Flight 145 started in the Ariane 5 launcher integration building, when the core cryogenic stage was erected and mated to Ariane 5’s two solid boosters.
On September 19, 2001 an EPS storable propellant upper stage was installed atop the core stage, allowing the basic integration process to be completed. This upper stage subsequently is to be replaced by another that incorporates modifications adopted after the in-flight malfunction that occurred during Flight 142.
The S5 satellite preparation facility at Europe's Spaceport is alive with activity once again as Envisat enters its final checkout in preparation for launch in late February. This large Earth monitoring spacecraft will be orbited by the next Ariane 5 mission (Flight 145), set for late February.
The Envisat satellite includes a large side-mounted solar panel that will serve the spacecraft's average power requirement of 3,560 Watts. The solar panel and antennas on Envisat will deploy after launch by Ariane 5, giving the spacecraft an in-orbit size of 26 X 10 X 5 meters.
January 10: Envisat takes shape in the S5 facility

The following photo show the action as Envisat's solar array was moved into position for integration on the spacecraft's service module. The solar array is made up of 14 panels and provides 6.5 kW of power at end-of-life. When deployed in space, the array will measure 14 meters × 5 meters.

February 7: Envisat is readied for fueling:
While Envisat is one of the largest satellites built by Europe, it is accommodated with ease in the S5A fueling and integration hall of the S5 facility. In this picture, personnel conduct tests in preparation for the satellite's fueling with monopropellant hydrazine. After its February 28 launch, Envisat will be operated by the European Space Agency to monitor the Earth and its environment in unprecedented detail.
A system control check is performed as preparations are made for fueling of the Envisat spacecraft in the S5A hall. Envisat has a maximum overall mass of 8,500 kg. at launch, and will be filled with a nominal propellant load of 314 kg. of monopropellant hydrazine, which is to be carried in four tanks of the propulsion subsystem.
The satellite makes its first contact with launcher hardware! Envisat is mated to the Ariane 5's payload adapter. The adapter will be the interface between the spacecraft and its Ariane 5 when the payload is installed atop the heavy-lift launch vehicle. As preparations with Envisat continue inside the S5 building, the launcher is undergoing final checkout in the Ariane 5 final assembly building several kilometers away.

Mission report:



Astrophilately covers:

Ariane-511

Launch cancel Kourou

Ariane-511

Headquarter cancel Paris

Credit covers: J.VdDr.

Ref.: #7, #15, #66a, #97, #226, #415 - update: 05.11.19 Home