ADCS & Navigation — Space Hardware Marketplace

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.

Attitude Control Module PnP ADCS-N1

• Star Tracker - Quantity2
• Star Tracker - Accuracy (Pointing/Rolling)5" (3sigma) / 50" (3sigma)
• Star Tracker - Update Rate10 Hz

A plug-and-play (PnP) satellite attitude determination and control module (ADCS-N1) integrating star trackers, sun sensor, gyroscope, magnetometer, reaction…

NST10-G1 Star Tracker

A fully autonomous Nano Star Tracker offering high precision attitude determination with high dynamic performance of 10 deg/s,…

NST20-G2 Star Tracker

An upgraded, fully autonomous, highly reliable, precision high-dynamic star tracker with 20 deg/s dynamic performance and a secondary…

NST20-G3 Star Tracker

A fully autonomous, highly reliable, high-precision and high-dynamic attitude star tracker, upgraded from the NST10-G1, delivering 1 arcsec…

NST4S-A2 Star Tracker

An autonomous Nano Star Tracker for high-accuracy attitude determination, with more than 50 units flight-proven on orbit.

NST5S-A1 Star Tracker

An autonomous, high-precision and compact star tracker upgraded from the NST4S-A2, featuring a wide 35-degree Sun Exclusive Angle.

SS-D Sun Sensor

The SS-D Sun Sensor is a high-accuracy digital sun sensor that outputs a 2-axis sun vector angle for…