STIM210 MEMS Gyroscope Module
Compact tactical-grade MEMS gyroscope module with 0.3 deg/hr bias stability, LEO-proven on over 30 satellite programs since 2012.
Typed specifications6 values
Discloses 4 of 11 fields engineers filter by in this category (category median 3).
- Mass
- 52 g product page
- Bias instability
- 0.3 °/h product page
- Angle random walk
- 0.15 °/√h product page
- Power consumption
- 1.3 W product page
- Radiation tolerance (TID)
- 5–7 krad product page
- Flight heritage
- 30+ satellite programs since 2012 product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier7 lines, in the manufacturer's own wording
- Bias stability
- 0.3 deg/hr
- Arw
- 0.15 deg/sqrt(h)
- Mass
- 52 g
- Power
- 1.3 W
- Radiation tolerance
- 5-7 krad TID
- Flight heritage
- 30+ satellite programs since 2012
- ITAR
- Free
About
The STIM210 (developed by Safran Sensing Technologies Norway / Sensonor) is a compact, tactical-grade MEMS gyroscope module providing up to 3 axes of angular rate measurement. With 52 g mass and 1.3 W power consumption, it is CubeSat-compatible. The STIM210 has been in continuous LEO operation since 2012 on over 30 different satellite programs, making it an industry standard for small satellite attitude control. Radiation tolerance of 5-7 krad TID for LEO qualification. ITAR-free.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.