ADCS & Navigation — Space Hardware Marketplace

Antenna-feeder system of global navigation satellite systems

A passive printed L1-band antenna (AFS-GNSS) for receiving GNSS positioning signals aboard a spacecraft.

piMAGGYRO

• TypeDigital CubeSat tri-axial magnetometer and gyroscope
• Magnetic field range+/- 300,000 nT per axis (0-519,615 nT total magnetic field maximum range)
• Magnetic field resolution6 nT resolution, 35 nTrms noise (total magnetic field)

Non-deployable tri-axial digital CubeSat magnetometer and gyroscope with telemetry engine for in-situ magnetic field and tumbling rate measurement.

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.

piMAGGYRO

Non-deployable digital tri-axial CubeSat magnetometer and gyroscope with telemetry engine, 10 Hz update rate over UART.

piPATCH-AllBand-TC

Active All-Band CubeSat GNSS patch antenna covering GPS L1/L2/L5, GLONASS G1/G2/G3, Galileo E1/E5a/E5b/E6 and BeiDou B1/B2a/B2b for Tuna-Can…

NANOadcs

High performance GNC platform for ADCS with built-in fault-tolerant OBC, GNSS, magnetometer and gyroscope.

3 Axis Attitude Control (Cyber Reaction Wheel)

• Momentum storage2.0 mNms (@19,000 rpm)
• Nominal rotational speed19,000 rpm
• Nominal torque0.1 mNm

Compact, cube-shaped reaction wheel with integrated electronics for single- and multi-axis attitude control of pico/nano satellites.

Lodestone

• Operating temperature-40 C to +85 C
• Dimensions22 x 20 x 6 mm
• Mass< 10 g

Compact combined magnetometer, gyroscope, and accelerometer module for nanosatellite attitude determination.

Zenith

• Operating temperature-40 C to +85 C
• Dimensions50 x 50 x 8.8 mm (customizable)
• Mass20 g

High-performance ceramic patch antenna for GNSS reception in nanosatellite missions.

Celeste

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

GNSS receiver providing precise positioning, navigation, and timing for CubeSat missions.

VANTAGESun

• Field of view (Coarse)<5 deg
• Field of view (Medium)<1 deg
• Field of view (Full Angle Circular)120 deg

Low-cost, low-mass, unpowered coarse sun sensor for initial spacecraft attitude acquisition.