31 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
CMG-10m is a variable-speed, single-gimbal Control Moment Gyroscope (CMG) which is suitable for 3U CubeSats. Unlike traditional CMGs…
ADCS-10m is an integrated ADCS with a variable-speed, single-gimbal Control Moment Gyroscope (CMG) which is suitable for 3U…
ADCS-20m is an integrated ADCS with two variable-speed, single-gimbal Control Moment Gyroscopes (CMG) which is suitable for 6U…
ADCS-40m is an integrated ADCS with four variable-speed, single-gimbal Control Moment Gyroscopes (CMG) which is suitable for 12U…
ADCS-MTQ uses a triaxial magnetometer and a triaxial magnetorquer for attitude control. Its control modes include magnetic dipole…
CMG-20m has two variable-speed, single-gimbal Control Moment Gyroscope (CMG) which is suitable for 6U CubeSats. Unlike traditional CMGs,…
CMG-40m has four variable-speed, single-gimbal Control Moment Gyroscope (CMG) which is suitable for 12U and 16U CubeSats. Unlike…
FSS-15 is a minimized fine sun sensor with a high cost-performance ratio. It is designed to be mass-produced…
Compact all-in-one Electrical Ground Support Equipment for testing and configuring Tensor Tech ADCS boards, CMGs, and FSS units.
High-dipole-moment magnetorquer rod for SmallSats, switchable 100/200 Am², optional PWM driving circuit.
Standalone magnetorquer rod with switchable dipole moment (10.45/20.81 Am²) and optional PWM driving circuit.
Standalone magnetorquer rod, 0.2 Am² dipole moment, 5 V input, compact form factor.
Integrated magnetorquer control board with two magnetorquers and one air coil, providing CubeSat detumbling and basic pointing.
Main control board / AOCS platform for real-time attitude estimation and control, interfacing with the spacecraft OBC.
Configurable inertial reference unit for satellite inertial sensing, with optional GNSS and magnetometer.
Ground test facility for ADCS calibration, mass-properties measurement, and algorithm validation: air-bearing platform, triaxial Helmholtz cage, and solar…
Configurable attitude and heading reference system with optional dual/single-antenna GNSS and embedded 3-axis magnetometer.
Ground-equipment attitude and heading reference system built on array-IMU technology using automotive-grade IMUs.
We use cookies. Strictly necessary cookies keep the platform working. With your consent we also use Google Analytics to understand how the platform is used and improve it. We do not use advertising cookies. Cookie Policy · Privacy
Favorites are available to clients only. Sign in to your client cabinet or create a free account — it takes less than a minute.
How is your experience with the platform? Your message goes straight to our team.
Thank you! Your feedback has been sent to our team.
