Aerospace Systems
Earth Sensors
Global Positioning Systems
Momentum / Reaction Wheels
Satellite Communication Antennas
Star Cameras
Sun Sensors

Star Cameras

Used on space station Mir and the International Space Station. Utilizes RAD hardened electronics.

Quality

Probability of failure free operation during a 100 hour session:

 VF STC 1VF STC 2
Mass electronics + baffle3.2 kg3.4 kg
Power10.2 Watts5.0 Watts
Input Current24 to 28 Volts24 to 28 volts
Accuracy (x,y)3 arc seconds3 arc seconds
Accuracy (z)15 arc seconds22 arc seconds
Field of View8 degrees circular160 x 160
Star Catalog8,500 selected from 100,000~5,000
Search Time (Initial)30 seconds30 seconds
Search Time2 seconds2 seconds
Maximum Star Magnitude+8.5+ 6
Dimensions mm320 x 320 x 160280 x 280 x 225
Rad Hardened MicroprocessorYesYes
Lifetime15 years15 years
Focal Length60 mm35 mm
Aperture-16 mm
OutputQuaternionQuaternion
CCD Array512 x 512 pixels-
InterfaceMil 1553 BMil 1553 B
Lenses58
LanguageC+ or C++C+ or C++

Full Quality Testing

All Valley Forge units can be modified to your specifications.