Spot 4
The total cost of the satellite over 6 years (contruction, launch,
exploitation) is approx. $500 million
http://spot4.cnes.fr/
sat-index articles
Prime
contractor
|
Matra
Marconi Space
|
Platform
|
Spot
Mk 2
|
Mass
at launch
|
2755
kg
|
Dry
mass
|
2600
kg
|
Payload
mass
|
1390
kg
|
Dimension
|
2.5
x 2.5 x 5.35 m
|
Solar
array
|
4
x 8 m
|
Stabilization
|
3-axis
|
DC
power
|
EOL:
2200 W
|
Design
lifetime
|
5
years
|
Telemetry: 1704 MHz
Telemetry: 2218 MHz (4096 kbps)
Telemetry: 8253 MHz
Command: 2042.408 MHz (2 kbps)
Command: 5690 MHz
Wavebands
|
0.50-0.59
µm (green)
0.61-0.68 µm (red)
0.79-0.89 µm (near IR)
1.53-1.75 µm (mid-IR)
|
Swath
width
|
60
km (each HRV)
|
Resolution
|
Monospectral:
10 m
Multispectral: 20 m
|
CCD with 6000 points. Has the same on-board recorder as
Helios 1A
provided by Enertec (2 x 120 Gbits). HRVs are steerable to either side of the
ground track (+/- 27°) to provide re-visits and stereoscopic images
Wavebands
|
0.43-0.47
µm (blue)
0.61-0.68 µm (red)
0.78-0.89 µm (near IR)
1.58-1.75 µm (mid-IR)
|
Swath
width
|
2000
km
|
Resolution
|
1.15
to 1.7 km
|
Vegetation monitoring Instrument. Onboard storage: 2.25 Gbit
The PASTEL system (
PAssager Spot de TElécommunication Laser) use
the SILEX (Semiconductor Intersatellite Link Experiment) payload to downlink via
Artemis
at 50 mpbs. The link is operated at optical frequencies at a wavelength of 800
to 860 nanometers. The light source is a solid state laser diode operated
typically at 60 mW optical power. The applied modulation scheme is direct
intensity modulation. A photo diode is used as optical data detector.
The difficulty involves aligning and stabilizing two terminals which are on
average 38 500 km away from each other, with a pointing error of less than 2
micro-radians. In other words, the beam from PASTEL (which at that distance,
would have a diameter of 200 m) would have to be kept centred on OPALE with a
tolerance of +/- 38m. This is equivalent to to hitting an orange with a rifle
shot from 51 km!