VIONICS SPACE SATELLITE CAMERAS

The Vionics Orbital Express uncooled infrared and visible satellite cameras underwent rigorous thermal and vibration finite element analysis as well as comprehensive verification testing to ensure high reliability operation.

Thermal finite element modeling
and analysis
Thermal vacuum and cycling testing
and burn in
Vibration finite element modeling
and analysis
Random vibration testing
Operational reliability in space is provided through protective recovery circuits that handle radiation induced upset, latch up events, and the use of space qualified components.
Parameters - Infrared camera (without lens)
Size
3.8” W x 4.5” L x 4.5”H
Weight
3 lbs 2.2 oz.
Current (typ)
230 mA @ 28VDC
Infrared sensor
320 x 240
Parameters - Visible camera (without lens)
Size
3.8”W x 4.5”L x 4.5” H
Weight
3 lbs .5 oz.
Current (typ)
248 mA @ 28VDC
Visible sensor
1024 x 1024
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