SUN
SENSORS

Model 0.5
Features:
±0.5° Two axis sun readout accuracy over 100° field of view
Earth Albedo error minimization
Weight: less than 40 grams
Power: less than 50 mwatts or zero watts if ±1° albedo
error is acceptable
Reliability: greater than 0.999 for a 15 year mission
Active parts complement comprises only one quad op-amp
S-level parts available with quantity orders
Suitable for LEO, GEO, or interplanetary applications
Proprietary signal processing software incorporated
into spacecraft computer, requiring less than 100 kbytes of memory
± 5 to ±15 volt power input
Qualified for 2006 flight in CUBESAT spacecraft:
-30°c to +80°c thermal vacuum (3 cycles)
0.16 g2/hz. 50-800 Hz. Random vibration
Extremely cost effective price: $16,000- each

Model 0.05
Features:
±0.5° Two axis sun readout accuracy over 100° field of view
This accuracy achieved with patented
detector/amplifier drift compensation
Earth Albedo error minimization
Weight: less than 40 grams
Power: less than 50 mwatts
Reliability: greater than 0.999 for a 15 year mission
Active parts complement comprises only one quad op-amp
S-level parts available with quantity orders
Suitable for LEO, GEO, or interplanetary applications
Proprietary signal processing software incorporated
into spacecraft computer, requiring less than 100 kbytes of memory
±5 To ±15 volt power input
Extremely cost effective price: $40,000- each
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