Dong Fang Hong 45

China


Spacecraft n°:

Chinese spacecraft n°: 54

Also called Feng Yun 2B or Feng Yun 2-1R (some incorrectly name it 2A)

Launch data:

Designation 24834 / 97029A
Launch date 10 Jun 1997
Launch site Xichang, LC-1
Launch vehicle  CZ-3
MissionMeteorology
Geostationary orbit 105°E

First Chinese GEO meteorology satellite. The 1R and B denomination stands for the replacement of the original satellite destroyed before even being installed on the Long March and launched, in 1994.

The satellite is equipped with a scanning radiometer, a cloud coverage information system and a data collection and transmission system.

Specifications

Prime contractor Shanghai Aerospace Technology Research Institute
Platform  
Mass at launch 1380 kg
Mass in orbit  
Dimension cylinder: 2.1 m x 1.6 m
Solar array  
Stabilization spin-stabilized (100 rpm)
DC power  
Design lifetime 3 years

The satellite is said to be a copy of GMS 5

End of life

Out of service April 1998
Cause failure of the S-band antenna mechanism


VISSR (Visible and IR Spin Scan Radiometer)

Wavebands 0.55-1.05 µm (visible)
6.2-7.6 µm (water vapour)
10.5-12.5 µm (IR)
Resolution visible: 1.25 km
IR& WV: 5 km
Image repeat frequency 1 hour

Downlink: 1687.5 MHz linear (PCM/BPSK, 660 kbps)

Ref: #15 - update: 13.03.10