Image of Optical Energy Technologies  - Sun Sensors for Spacecraft on the satsearch marketplace

Key highlights

Features:

Sun-Sensor-Model-1-350w-2±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

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Last updated: 2020-04-17

Sun Sensors for Spacecraft

Image of Optical Energy Technologies  - Sun Sensors for Spacecraft on the satsearch marketplace

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