Tensor Tech (thermal)

Manufacturer TWN Verified
23 Products
7 Years Active
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About Tensor Tech (thermal)

Tensor Tech Co., Ltd. is a Taiwanese spacecraft attitude determination and control (ADCS) company headquartered in New Taipei City, Taiwan, with a US office in San Jose, California, developing flight-proven space-qualified ADCS products ranging from complete integrated systems to individual components for nanosatellites and small satellites. The company's product portfolio includes Control Moment Gyroscopes (CMG), sun sensors, magnetorquers, integrated ADCS systems for NanoSat and SmallSat platforms, ground support equipment, and mass properties analysis tools, all backed by an ISO 9001-certified quality management system and rigorous testing. Tensor Tech provides scalable ADCS solutions — ranging from miniaturised attitude sensors for 1U CubeSats to complete multi-mode ADCS for larger platforms — targeting academic, institutional, and commercial small satellite developers seeking reliable, flight-proven attitude control hardware.

Products

23

Ground test facility for ADCS calibration, mass-properties measurement, and algorithm validation: air-bearing platform, triaxial Helmholtz cage, and solar simulator.

2 17

Configurable attitude and heading reference system with optional dual/single-antenna GNSS and embedded 3-axis magnetometer.

1 12

1-axis analog coarse sun sensor with 5-degree (1-sigma) accuracy for sun-acquisition and low-pointing-requirement missions.

3 6

Ground-equipment attitude and heading reference system built on array-IMU technology using automotive-grade IMUs.

2 12

Configurable inertial reference unit for satellite inertial sensing, with optional GNSS and magnetometer.

1 12

Integrated CMG-based ADCS for nanosatellites up to 30 kg, mounting in a single tuna-can occupying 0.25U.

3 12

3-axis discrete CMG-based ADCS for nanosatellites up to 30 kg with 11.7 mNms momentum capacity.

2 12

High-momentum 3-axis discrete CMG-based ADCS for nanosatellites up to 30 kg, 36.4 mNms capacity.

2 12

Magnetorquer-only basic ADCS variant for detumbling and coarse pointing on nanosatellites.

1 8

Main control board / AOCS platform for real-time attitude estimation and control, interfacing with the spacecraft OBC.

1 2

Variable-speed, single-gimbal Control Moment Gyroscope for SmallSats, 1 Nms momentum, single or clustered configuration.

1 13

Variable-speed, single-gimbal Control Moment Gyroscope for SmallSats, 10 Nms momentum, single or clustered configuration.

1 13

Variable-speed, single-gimbal Control Moment Gyroscope for CubeSats up to 16U and nanosatellites up to 30 kg — skew-mount version.

2 12

Variable-speed, single-gimbal Control Moment Gyroscope for CubeSats up to 16U and nanosatellites up to 30 kg — vertical-mount version.

2 12

Variable-speed, single-gimbal Control Moment Gyroscope for SmallSats, 4 Nms momentum, single or clustered configuration.

1 13

Compact all-in-one Electrical Ground Support Equipment for testing and configuring Tensor Tech ADCS boards, CMGs, and FSS units.

1 6

Fine sun sensor based on a photodiode quadrant detector, up to 0.1-degree accuracy, with optional embedded tri-axis magnetometer.

2 10

Discrete-optics fine sun sensor, 100 krad.

1 10

Fine sun sensor with embedded tri-axis magnetometer, < 0.1-degree accuracy, 5 V input.

1 10

Integrated magnetorquer control board with two magnetorquers and one air coil, providing CubeSat detumbling and basic pointing.

2 8

Standalone magnetorquer rod, 0.2 Am² dipole moment, 5 V input, compact form factor.

1 8

Standalone magnetorquer rod with switchable dipole moment (10.45/20.81 Am²) and optional PWM driving circuit.

1 8

High-dipole-moment magnetorquer rod for SmallSats, switchable 100/200 Am², optional PWM driving circuit.

1 8

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