Adeos 1
Advanced Earth Observing Satellite, also called Midori (means
"green")
To acquire global observation data corresponding to enviromental changes, such
as global warming, depletion of the ozone layer, decrease of tropical rain
forests, occurrence of unusual weather, etc. it will also help develop the
platform bus interorbit data relay technologies necessary for next-generation
Earth Observation Systems.
The satellite encountered several problems after launch: first a thruster
problem which required to use the 20 N adjusters to reach final orbit; then on
24th September 1996 the satellite shutdown all nonessential systems. At the
same time a scanning mirror used by the Interferomic Monitor for Greenhouse
Gases became stuck on 20 September. Also, it was found that cosmic radiations
affected the on-board computer. In late 1996 it was also found that the OCTS
instrument has a mirror blocked.
Satelite cost: $474 million
http://jwocky.gsfc.nasa.gov/adeos/adeos.html
http://www.eorc.nasda.go.jp/ADEOS/
sat-index articles
Out
of service
|
30
Jun 1997
|
Cause
|
electrical
failure caused by the solar array paddle break itself caused by improper maneuver
|
Prime
contractor
|
Mitsubishi
|
Platform
|
|
Mass
at launch
|
3500
kg
|
Mass
in orbit
|
|
Dimension
|
4
x 4 x 5 m
|
Solar
array
|
3
x 26 m
|
Stabilization
|
3-axis
|
DC
power
|
4500
W
|
Design
lifetime
|
3
years
|
Telemetry/data at: 2220, 8150, 8250, 8350 MHz perhaps also 467.7 MHz?
Ka-band inter orbit links to
Comets
Ocean Color and Temperature Scanner (OCTS)
Advanced Visible and NearInfrared Radiometer (AVNIR)
NASA Scatterometer (NSCAT)
Total Ozone Mapping Spectrometer (TOMS)
Polarization and Directionality of the Earth's reflectances (POLDER)
Interferometric Monitor for Greenhouse Gases (IMG)
Improved Limb Atmospheric Spectrometer (ILAS)
Retroreflector in Space (RIS)