Space Hardware Marketplace

TensorEGSE

• Dimensions164 x 96 x 27 (H) mm3
• Available Controlled Power Supply Line3.3 V, 5 V
• InterfaceUART, RS-485, RS-422/CAN

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

TensorMTQ-200

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

TensorMTQ-20

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

TensorMTQ-2

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

TensorMTQ Board

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

TensorAOCS-MCB

• InterfacesRS-422, RS-485, UART, I2C, SPI, CAN-FD, Ethernet, SpaceWire, and MIL-STD-1553
• Radiation tolerance> 24 krad(Si) on electronics

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

ADCS Testbed

• Air-Bearing Platform — Position of Center of Mass, manually adjustable (X, Y, Z axes)25 mm (± 12.5 mm)
• Air-Bearing Platform — Turbine Torque5 μNm (typical)
• Air-Bearing Platform — Travel Angle< ± 12 deg for regular platform (Max. load 30 kg); < ± 22 deg for small platform (Max. load 10 kg)

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

IRU-ODM

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

AHRS-ODM

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

DynaSense AHRS

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

CSS-10 Coarse Sun Sensor

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

TensorFSS-30M Fine Sun Sensor

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

TensorFSS-30 Discrete Fine Sun Sensor

Discrete-optics fine sun sensor, 100 krad.

TensorFSS-15M Fine Sun Sensor

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

TensorCMG-10

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

TensorCMG-4

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

TensorCMG-1

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

TensorCMG-10m-V

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