ADCS & Navigation — Space Hardware Marketplace

Altitude Control System

• PurposeSpacecraft attitude control system
• Year of release2018
• Guaranteed service life (LEO)1 year

Compact ADCS (1 deg pointing, 0.1 deg knowledge, CAN/USB/BT interfaces) for small spacecraft, 2 W average power.

Retroreflector system for AC (spacecraft) Sentinel-3 (ESA)

• PurposeReflection of quantum-optical station radiation for precision spacecraft orbit determination
• Year of release2011
• HeritageFlown on ESA Sentinel-3 spacecraft

Seven-reflector retroreflector array for precision laser ranging of the ESA Sentinel-3 spacecraft.

Retroreflector system for “Luna-Globe” spacecraft

• PurposeRe-reflection of laser radiation for ground-to-spacecraft ranging
• Year of release2013
• HeritageDeveloped for Luna-Globe lunar mission

Interference-coated angle-reflector panel for laser ranging on the Luna-Globe lander/orbiter.

Retroreflector system “Pyramid” for “Condor-FKA” spacecraft

• PurposeRe-reflection of laser radiation toward ground station photodetector to calibrate onboard equipment
• Year of release2016
• HeritageDeveloped for Condor-FKA spacecraft

Compact four-reflector "Pyramid" retroreflector for onboard calibration on the Condor-FKA satellite.

Ring retroreflector system for “Glonass-K2” spacecraft

• PurposeMetrological control of GLONASS space-complex characteristics and calibration of ground measuring instruments
• Year of release2017
• HeritageDeveloped for GLONASS-K2 spacecraft

36-reflector ring panel for metrological control and calibration of the GLONASS-K2 navigation constellation.

Lens SOVA-5

Wide-angle 13-lens objective for detection of low-orbit space objects at altitudes from 120 to 500 km.

SX-SBOX ADCS Actuators (Microsatellite)

• ADCS control unit SX-SBOX-ADCU-01ARM Cortex-M4 160 MHz, hot-redundant, RTOS, ≤5 W, 220 g
• Reaction wheel SX-SBOX-RWH-50-2.0-01Max torque 0.05 N·m, momentum 2 N·m·s, 43 W peak, 3.2 kg
• Magnetorquers SX-SBOX-MTQSX-MT-1…SX-MT-30: dipole 1–30 A·m², 200–1200 g

Attitude-control actuators of the SX-SBOX suite for microsatellite platforms: ADCS control unit, reaction wheel, magnetorquers and a magnetorquer…

SX-SBOX ADCS Sensors (Microsatellite)

• Satellite navigation SX-SBOX-GNSS-01Position 10 m (σ), velocity 0.01 m/s, 2 W
• GNSS antenna SX-SBOX-AGG-011559–1607 MHz, gain ≥5.5 dB, RHCP, 61 g
• MEMS rate sensor SX-SBOX-AVS-MEMS-01Bias drift 2°/h, noise 0.15°/√h, 0.6 W, 75 g

Attitude-determination and navigation sensors of the SX-SBOX suite for microsatellite platforms: satellite navigation, GNSS antenna, MEMS and fiber-optic…

SXL-AIRTABLE-02 Spacecraft Relative-Motion Air Table

• TypeAir-bearing relative-motion table
• Overall dimensions5000 × 4000 × 3000 mm
• Active area1860 × 2480 mm

Air table for testing relative motion of spacecraft: a precision aluminium horizontal surface with an even grid of…

SXL-SCOE-SS-01 Sun Sensor Calibration Bench

• TypeSun-sensor calibration bench
• Rotary stage±100° vertical axis; unlimited horizontal axis
• Angle-setting accuracy0.002 °

Bench for calibration and verification of small matrix and diode-type sun sensors (linear and two-dimensional). The sensor is…

ADCS Hardware-in-the-Loop Simulation Bench

• TypeADCS hardware-in-the-loop bench
• SXC config 01CubeSat 1U/3U/6U; Helmholtz coils 2 m, Ø600 mm uniform field; air-bearing ≤ 35 kg; pointing accuracy ≤ 0.25°
• SXC config 02Educational; Helmholtz coils 1.3 m, Ø250 mm field; air-bearing ≤ 35 kg; accuracy ≤ 1°

Hardware-in-the-loop simulation bench for developing and verifying attitude determination, stabilization and navigation systems of small spacecraft under conditions…

SXC-SD-01 Sun Sensor

Sun sensor for nanosatellite attitude determination and control. The CAN interface allows a single sensor or a daisy-chain…

CubeSat Reaction Wheels Module SXC-FW4-02

4-flywheel reaction wheel module for 3U+ CubeSats. DC brushless motors with vacuum-rated bearings, CAN interface per driver, ±5000…

Reaction Wheels RW0 / 4RW0

• TypeReaction wheel actuator
• ConfigurationsRW0 single / 4RW0 cluster
• FunctionADCS / 3-axis attitude control

Momentum reaction wheels for CubeSat attitude control — single unit (RW0) or 4-wheel cluster (4RW0).

Onboard Computer (OBC)

Flight computer for SmallSats and CubeSats with 2x higher radiation resilience and ADCS-ready sensors. Low power consumption with…