- 4000 linear image sensor, PGA, 12 bit ADC output
- Destructive / Non destructive readout mode
- Global exposure control pin to control integration time
- Low fixed pattern noise, high dynamic range



- 256 x 512 area sensor, PGA, 12 bit ADC output
- 50 μm x 50 μm pixel size
- Snap shot function, up to 250 ms integration time
- Row wise response compensation, dark voltage cancellation
- < 1 % of the linearity

 

 

 


- 12,000 pixels of PAN and 6,000 pixels of four Multi-spectral (B, G, R, NIR)
- Extra high speed (0.3 ms / line integration time)
- 10 μm x 10 μm for PAN and 20 μm x 20 μm for Multi-spectral

 

 






Japan China India
USA
Satellite Kaguya Chang'e-1 Chandrayaan-1 Lunar Reconnaissance Orbiter
Overall Weight [tons]
3.0
2.3 1.4 -
Launch Date
September 2007
October 2007
October 2008
June 2009
Camera Type
Terrain Camera & Multi-band
3D Terrain Mapping
3D Terrain Mapping
3D Terrain Mapping
Sensor CCD CCD CMOS (C640)
CCD
Camera Weight [Kg]
9.4 > 30
6.3 9.8
Camera Power [Watts]

> 10
1.8 20




CCD
CMOS
< 100 krad
< 300 krad






Band
Band Definition [nm]
Mean Irradiance [W/m2]
Saturated Irradiance [W/m2]
SNR @ Mean Irradiance
PAN 400 ~ 700
0.1430 0.5460 ≥ 100
B1
455 ~ 515
0.0318 0.1193 ≥ 105
B2
525 ~ 595
0.0350 0.1402 ≥ 105
B3
630 ~ 690
0.0319 0.1239 ≥ 105
B4 762 ~ 897
0.0571 0.2445 ≥ 105


To learn more about our CMOS space sensors, please read the following information:

CMOS Sensor for RSI applications

Multi band CMOS Sensor simplify FPA design