Space Hardware Marketplace

NF-AMF Hexahedron (Near Field Antenna Measurement Facility)

• Maximum Scanning Area1.5 m x 1.5 m
• Scan Speed100 scan points, 5 cm spacing (10x10), in 4 minutes
• Scanning SystemHorizontal Planar Measurement System

Fully automated near-field antenna measurement system with anechoic chamber, 5 mm scan spacing and far-field projection.

VFF-AMF InnoWave 4 (Vertical Far Field Antenna Measurement Facility)

• Angular Precision0.45 deg
• Frequency RangeCustomisable
• Measurement Time (Per Plane)5 minutes

Vertical far-field antenna measurement facility for real-time antenna radiation pattern and gain measurement over the full frequency range.

HFF-AMF InnoWave 4 (Horizontal Far Field Antenna Measurement Facility)

• Angular Precision0.45 deg
• Frequency RangeCustomisable
• Measurement Time (Per Plane)5 minutes

Portable horizontal far-field antenna measurement facility delivering real-time 3D antenna radiation pattern and gain measurements.

AirSAR-Alpha-X

Multi-channel X-band SAR payload for airborne platforms, delivering ultra high-resolution imagery at 0.3-0.5 m resolution.

AirSAR-Alpha-L

Multi-channel L-band SAR payload for UAVs and aircraft, offering the world's highest resolution L-band foliage-penetrating imaging.

400 mNms Microsatellite Reaction Wheel

• Angular momentum capacity400 mNms
• Equivalent CMG performance0.4 Nms CMG at 22.5 deg/sec gimbal rate
• Target applicationHigh-agility remote sensing / science microsatellites

High-torque, radiation-hardened wheel for high-agility remote sensing or science microsatellites.

Sinclair Star Tracker (ST-16RT2)

• On-orbit heritage78+ units across SkySat, BRITE, GHGSat, Landmapper-BC, MKA-N, BlackSky Global, ALE, Momentus X-1, NEMO-HD and others
• Product typeStar tracker with integrated sun-baffle
• InterfaceSerial digital interface, quaternion attitude output plus telemetry

High-performance star tracker and baffle for small spacecraft, with 78+ units flown on more than a dozen missions.

3 mNms Picosatellite Reaction Wheel

• Angular momentum capacity3 mNms
• Form factor fit3 wheels per 1U CubeSat, or 4-wheel pyramid configuration
• Control interfaceDigital serial bus, commandable speed/momentum/torque

Sinclair's smallest reaction wheel — three units fit inside a 1U CubeSat, or four in a pyramid configuration.

10 mNms Picosatellite Reaction Wheel

• Angular momentum capacity10 mNms
• On-orbit heritage10 units on 4 spacecraft (first launch June 2014)
• Target applicationSmall CubeSats

Small reaction wheel ideally suited for smaller CubeSats, with 10 units flown on 4 spacecraft.

30 mNms Nanosatellite Reaction Wheel

• Angular momentum capacity30 mNms
• On-orbit heritage61 units on-orbit (first launch April 2008)
• Form factor fit6U to 12U CubeSat

Sinclair Interplanetary's first and most popular wheel design, sized to fit a 6U to 12U CubeSat.

60 mNms Microsatellite Reaction Wheel

• Angular momentum capacity60 mNms
• On-orbit heritage68 units on 20 spacecraft (first launch June 2014)
• Motor driveHigh-torque motor phase current control electronics

Compact high-torque wheel packing motor phase current control electronics into a small package.

1 Nms GEO Reaction Wheel

• Angular momentum capacity1 Nms
• Target orbitGEO / high-radiation orbits
• Radiation hardeningRad-hard parts, shielded enclosure, active deep-charging mitigation

Radiation-hardened version of the heritage 1 Nms wheel, built for GEO and other high-radiation orbits.

1 Nms Microsatellite Reaction Wheel

• Angular momentum capacity1 Nms
• Target spacecraft class~100 kg Earth-observation microsatellite
• On-orbit heritage76 units on 19 spacecraft (first launch June 2016)

Sinclair Interplanetary's largest reaction wheel, suitable for 100 kg-class Earth-observation microsatellites.

Training, Operations, Mission Simulation (TOMS)

• Use casesOperator training, mission profile validation

Simulation used for operator training and for validation of the mission profile against client requirements.

Digital Twin

• Data sourceReal-time telemetry and other sources
• Use casesOperations optimization, risk mitigation, virtual prototyping, predictive maintenance

Digital twins of physical systems, fed by real-time telemetry, for operations optimization and risk mitigation.

Hardware In The Loop (HIL) Dynamic Simulation

• Integration targetOn-Board Computer (OBC) and other hardware components
• Validated functionEmbedded flight software / GNC module

Real-time hybrid simulation integrated with the OBC and other hardware components for embedded software validation.

Flight Software Development Dynamic Simulation

• Modeled scopeHardware ICDs for all relevant components
• CapabilitiesSend telecommands, receive telemetry

High-fidelity dynamic simulation for validating flight software and GNC in a purely digital environment.

Hardware Interface

• Supported buses/interfacesRS-232, RS-422, RS-485, CAN BUS, I2C, SpaceWire, PWM, SPI, Digital I/O, Analog inputs, Analog outputs, RTD, ARINC-429, ARINC-575, MUX BUS 1553

Ready-to-use hardware interface drivers for common aerospace hardware buses and interfaces.