C640 for 3D Terrain Mapping Camera (TMC)
C650 for Hyper-Spectral Imager Camera (HySI)
C468 for CMOS MSOC
Moon Missions
| 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 |
Radiation
| CCD | CMOS |
| < 100 krad | < 300 krad |
Focal Plane Array (Space Camera)
SNR Requirements
| 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 |