
Key highlights
Lens R&D's MAUS is a fine sun sensor, especially developed for the CubeSat and small satellites market, taking advantage of the BiSon64-ET development experiences, while maintaining focus on the special requirements for small satellites.
The sensor is designed to combine a high radiation tolerance, as needed for interplanetary missions (tested to be > 9Mrad), with the low profile required for efficient mounting on CubeSats.
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Last updated: 2024-08-27
MAUS Sun Sensor

Technical specs
field of view
±57.5° ±2° on axis
±65.8° ±2° in diagonal
±65.8° ±2° in diagonal
accuracy
<0.5 degrees 3σ (using calibration tables)
<2 degrees (using specific correction parameters)
<3.5 degrees (without calibration)
<2 degrees (using specific correction parameters)
<3.5 degrees (without calibration)
mass
< 15 g
operating temperature
-40 to 80 C
-45°C to +105°C (2000 TVAC cycles qualification)
-45°C to +105°C (2000 TVAC cycles qualification)
storage temperature
0 to 30 C
first frequency
> 200 Hz
mechanical shock
3000 g
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