ADCS & Navigation — Space Hardware Marketplace

NewSpace GNSS Receiver

• TypeMulti-constellation GNSS receiver
• ConfigurationsSINGLE, DUAL, TIMING, DB
• Product ClassNewSpace

NewSpace multi-constellation GNSS receiver for CubeSat and small satellite position, navigation, and timing applications.

RLT-GNSS-x Receiver Kit

• InterfacesRS232, 100 Mbps Ethernet
• ChannelsSingle (1-channel) or Dual (2-channel)
• ParametersPosition, velocity, timing/sequencing

Modular integrated GNSS receiver kit for launch vehicle telemetry.

GNSS Receiver Module (GPSRM 1) Kit

Pumpkin's flight GNSS receiver module for CubeSats, built around a NovAtel OEM719-series 555-channel space-grade receiver with dual selectable…

SpaceTech CESS (Coarse Earth Sun Sensor)

• Sensor principlePassive thermo-optical Coarse Earth and Sun Sensor
• Power consumptionZero power consumption
• Configuration6 orthogonally accommodated CESS heads to determine relative earth and sun vector

Passive thermo-optical Coarse Earth and Sun Sensor providing spacecraft attitude information during de-spin and safe mode.

SGR-Ligo Space GNSS Receiver

• Dimensions92 x 87 x 12 mm
• Power at 5V<0.5 W
• Mass90 g

Miniaturised CubeSat PC-104 standard Space GNSS receiver for LEO position, velocity and time.

SGR-Axio Space GNSS Receiver

Space GNSS receiver for small to larger satellites, successor to SGR-10, with multi-GNSS and dual-frequency options.

SSTL GEO Wheel (SSW-200)

Geostationary-orbit reaction wheel with 15 year design life, qualified with Airbus Defence and Space and ESA.

SSW-110 Reaction Wheel

Flight-proven low Earth orbit reaction wheel with fully integrated electronics, flown on 40+ missions.

ADCS control unit

• Dimensions, mm101 x 100 x 20 (without fasteners)
• Mass, g220
• Power voltage, V6-36 (without galvanic isolation)

A dual-redundant attitude control and stabilization system control unit (OSSCU, SX-SBOX-ADCU-01) running SPUTNIX's flight-qualified ADCS software.

Reaction wheel

• Dimensions, mm160 x 160 x 80 (without fasteners)
• Mass, kg3.2
• Power voltage, V22-34 (without galvanic isolation)

A control flywheel motor (CFM, SX-SBOX-RWH-50-2.0-01) generating control torque via rotor acceleration/deceleration for larger satellite platforms.

Magnetic torquers

• Model SX-MT-1Maximum moment 1 A*m2, Consumption 0.4 Wt, Mass 200 g, Diameter 16 mm, Dimensions 140x30x30 mm
• Model SX-MT-5Maximum moment 5 A*m2, Consumption 0.6 Wt, Mass 350 g, Diameter 20 mm, Dimensions 220x50x35 mm
• Model SX-MT-10Maximum moment 10 A*m2, Consumption 0.7 Wt, Mass 550 g, Diameter 20 mm, Dimensions 320x50x35 mm

A family of proprietary magnetic torquer rods (SX-MT-1 through SX-MT-30) used with the magnetic torquers control unit for…

Magnetic torquers control unit

• Dimensions, mm54 x 48 x 20 (without fasteners)
• Mass, g85
• Power voltage, V6-36 without galvanic isolation

A control unit (SX-SBOX-MTQU-01) driving up to three magnetic torquers via PDM channels to implement angular velocity damping…

Magnetometer

• Dimensions, mm54 x 52 x 16 (without fasteners)
• Mass, g70
• Power voltage, V6-36 without galvanic isolation

A triaxial anisotropic-magnetoresistive magnetometer (SX-SBOX-MAG-01) used in attitude determination alongside magnetic torquers for detumbling and momentum unloading.

Solar sensor

• Dimensions, mm43 x 43 x 16 (without fasteners)
• Mass, g45
• Power voltage, V6-36 without galvanic isolation

A compact sun sensor (SX-SBOX-SUNS-01) for the attitude control loop, with algorithms mitigating Earth-albedo glare, suitable for microsatellites…

Fibre-Optic Gyroscope

• Dimensions of the sensor unit275 x 275 x 160 mm (without fasteners)
• Dimensions of the control unit171 x 111 x 44 mm (without fasteners)
• Power voltage, V22-34, galvanic isolation 500V

A high-precision fibre-optic gyroscope (FOG, SX-SBOX-AVS-FOG-01) with a control unit and 4-element sensitive assembly (3 main + 1…

Satellite navigation equipment

• Dimensions, mm171 x 111 x 51 (without fasteners)
• Mass, kg0.7
• Power voltage, V22-34, galvanic isolation 500V

A GNSS receiver unit (SX-SBOX-GNSS-01) providing precision position, velocity and time synchronization for the spacecraft.

Angular velocity sensor

• Dimensions, mm54 x 52 x 20 (without fasteners)
• Mass, g75
• Power voltage, V6-36 without galvanic isolation

A triaxial MEMS-based angular velocity sensor (SX-SBOX-AVS-MEMS-01) for small satellite attitude determination.

Reaction wheels module

A 4-flywheel reaction wheel module (SXC-FW4-02) for CubeSat 3-axis attitude control, integrating drivers and control electronics on a…