449 satellite platforms, components and ground equipment from manufacturers worldwide.
The TensorFSS-15M is a 2-axis digital fine sun sensor for satellite attitude determination, offering 0.2-degree accuracy and low…
High-precision 2-axis digital fine sun sensor with 120° FOV and sub-0.2° accuracy, featuring an embedded calibration table and…
The TensorCMG Series features variable-speed, single-gimbal Control Moment Gyroscopes (CMGs) driven by spherical motor technology, suitable for satellites…
The TensorCMG-10m is a variable-speed, single-gimbal Control Moment Gyroscope (CMG) designed for CubeSats up to 16U and nanosatellites…
The TensorADCS series provides attitude determination and control systems for nanosatellites up to 30 kg, incorporating variable-speed, single-gimbal…
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.
TensorADCS is a configurable attitude determination and control system for nanosatellites up to 30 kg, using variable-speed single-gimbal…
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.
ARGO2.0 is a compact, scalable multi-camera Star Tracker System designed for small platforms, including CubeSats, offering high accuracy…
A modular family of space-qualified reaction wheels from VECTRONIC Aerospace, spanning 0.2 Nms to 8 Nms angular momentum,…
The VST-series star trackers are high-performance attitude determination sensors for small satellites, offering radiation tolerance and suitable for…
Compact low-momentum reaction wheel for small satellites, 0.2 Nms angular momentum.
World's smallest and lightest GNSS receiver module, developed for use on small satellites.
Attitude Control System expansion board for the Q7 processor, providing ACS interfaces, H-bridge drivers, and power switching.
Three-axis, low-dipole superconducting magnetic actuator for LEO spacecraft and space station attitude control, a solid-state alternative to CMGs.
Single-axis, ultra-high-dipole superconducting magnetic torquer delivering fuel-free attitude control authority for MEO/GEO spacecraft.
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