Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Envisat
Part of SPOT-4
Envisat
Envisat
Credit: Manufacturer Image
European earth resources radar satellite. The European Space Agency's Envisat polar platform was originally envisaged as an automated polar orbiting segment of the Space Station. Earth observation satellite built by Astrium for ESA, Europe. Launched 2002. Used the PPF/SPOT Mk.2 bus.

Status: Operational 2002. First Launch: 2002-03-01. Last Launch: 2002-03-01. Number: 1 . Gross mass: 7,911 kg (17,440 lb). Unfuelled mass: 7,611 kg (16,779 lb).

It was later descoped to become something like the European equivalent of NASA's Earth Observing System. Envisat used a new modular satellite bus built at the defunct Matra Marconi Space/Bristol. Final integration was done at ESTEC in the Netherlands. The service module (SVM) was based on the SPOT 4 design. Prime contractor was Astrium (Dornier). Envisat carried 300 kg of hydrazine monopropellant for orbital adjustments. The active C-band phased array ASAR radar imaging antenna was 1.3 x 10 m in size. Envisat also carried atmospheric radiometers and spectrometers and a radar altimeter.

Envisat was an advanced polar-orbiting Earth observation satellite which provided measurements of the atmosphere, ocean, land, and ice over a five year period. The Envisat satellite had an ambitious and innovative payload that ensured the continuity of the data measurements of the ESA ERS satellites. The Envisat data supported Earth science research and allow monitoring of the evolution of environmental and climatic changes. The major driver for the Polar Platform/Envisat satellite configuration was the need to maximize the payload instrument mounting area and to meet the viewing requirements within the constraints of the Ariane 5 fairing and interfaces. Additionally, the configuration was driven by the reuse of the SPOT Mk II service module concept and the ERS payload accommodation concept (instrument electronics in an internal enclosure with externally mounted antennas).

In flight, the major spacecraft longitudinal axis (the Xs-axis) was normal to the orbit plane, the Ys-axis was closely aligned to the velocity vector and the Zs-axis was Earth pointing. This configuration concept provided a large, modular, Earth-facing mounting surface for payload instruments and an anti-sun face for radiative coolers, free of occultation by satellite subsystem equipment.

Specification

The Envisat instruments span the electromagnetic spectrum from microwave to ultraviolet frequencies:


More at: Envisat.

Family: Earth, Civilian radarsat. Country: Europe. Launch Vehicles: Ariane 5, Ariane 5G. Launch Sites: Kourou, Kourou ELA3. Agency: ESA, Friedrichshafen. Bibliography: 2, 4, 550, 552, 554, 6479, 12317.

2002 March 1 - . 01:07 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5G.

Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use