TensorFSS-15M Fine Sun Sensor
Tensor Tech (thermal)Fine sun sensor based on a photodiode quadrant detector, up to 0.1-degree accuracy, with optional embedded tri-axis magnetometer.
186 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Fine sun sensor based on a photodiode quadrant detector, up to 0.1-degree accuracy, with optional embedded tri-axis magnetometer.
Variable-speed, single-gimbal Control Moment Gyroscope for CubeSats up to 16U and nanosatellites up to 30 kg — vertical-mount…
Variable-speed, single-gimbal Control Moment Gyroscope for SmallSats, 1 Nms momentum, single or clustered configuration.
High-momentum 3-axis discrete CMG-based ADCS for nanosatellites up to 30 kg, 36.4 mNms capacity.
Magnetorquer-only basic ADCS variant for detumbling and coarse pointing on nanosatellites.
Variable-speed, single-gimbal Control Moment Gyroscope for CubeSats up to 16U and nanosatellites up to 30 kg — skew-mount…
Integrated CMG-based ADCS for nanosatellites up to 30 kg, mounting in a single tuna-can occupying 0.25U.
3-axis discrete CMG-based ADCS for nanosatellites up to 30 kg with 11.7 mNms momentum capacity.
Attitude-control reaction wheel module for the ChallengeOne satellite platform, part of its Attitude Determination and Control System (ADCS).
Cyclops is a software-only visual positioning system (VPS) that gives fixed-wing UAVs reliable position estimates when GPS is…
Attitude determination and control sensors/actuators for nanosatellite pointing and orientation.
VISION/INS integrated navigation system assisted by GNSS, for on-orbit servicing missions.
Multi-camera star tracker system with up to five 4Mpixel cameras and a router and power control unit.
Compact multi-camera star tracker system with up to three 4Mpixel cameras and one electronics unit.
Low-SWaP integrated tri-axis magnetometer and dual-axis sun sensor for precise small satellite attitude determination.
Precision reaction wheel providing more than 2 Nms of momentum for small satellite attitude control, designed for NASA-compliant…
Compact magnetic torque rod delivering at least 6 Am² dipole moment for small satellite attitude control.
High-performance D-series reaction wheel with 6 Nms angular momentum.
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