ADCS & Navigation — Space Hardware Marketplace

SASC (Sub-Arcsecond Star Camera)

• Full-loss accuracy< 1 arcsec @ 10 Hz
• Differential precision0.23 arcsec @ 60 Hz
• InterfacesGigE, RS-232/485

A high-precision star camera used for attitude determination, delivering sub-arcsecond accuracy for spacecraft and high-altitude balloon platforms.

AHP54510 Levity Series Active L1/L5/L-Band GNSS High Precision Antenna

• ModelAHP54510.07.0100C
• GNSS typeActive
• BandsL1/L5/L-Band

Active multi-band L1/L5/L-Band GNSS antenna enabling centimeter-level correction-service positioning.

GVLB208 Series Ultra-Compact Dual-Band L1/L5 GNSS Antenna

• Dimensions20 x 20 x 8 mm
• GNSS bandsL1/L5 dual-band
• Peak gainup to 1.5 dBi

Ultra-compact 20mm dual-band L1/L5 GNSS antenna for centimeter-level positioning.

AHP5354A Active Multiband L1/L5 GNSS High Precision Patch Antenna

• GNSS typeActive
• GNSS bandsL1/L5
• Frequency range1176-1610 MHz

Multi-band active GNSS patch antenna delivering high-precision positioning for GPS/BeiDou/GLONASS/Galileo.

ChallengeOne Reaction Wheel

• Input voltage4-15 V
• Communication bus2x CAN2B; Battery UART
• Operating temperature-40 to +86 °C

Attitude-control reaction wheel module for the ChallengeOne satellite platform, part of its Attitude Determination and Control System (ADCS).

TensorMTQ-20

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

TensorMTQ-200

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

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.

TensorMTQ Board

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

TensorMTQ-2

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

AHRS-ODM

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

IRU-ODM

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

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.

DynaSense AHRS

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

TensorFSS-30 Discrete Fine Sun Sensor

Discrete-optics fine sun sensor, 100 krad.

TensorFSS-30M Fine Sun Sensor

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

TensorCMG-4

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

TensorCMG-10

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