ADCS & Navigation

AAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from satellite components to data analytics for various applications.

AAC Clyde Space

AAC Clyde Space RW210 Reaction Wheel

Low mass, low power CubeSat reaction wheel with fire-and-forget speed/torque control, available in 1.5, 3.0, or 6.0 mN.m.s momentum storage variants.

Total momentum storage	±1.5, ±3.0, or ±6.0 mN.m.s
Maximum torque	±0.1 mN.m
Maximum rotation rate	10000 / 15000 / 15000 rpm
Control accuracy	±0.5 rpm
Outer dimensions	25 x 25 x 15 mm

price on requestdatasheet

AAC Clyde Space

ANT-GPS Series

The ANT-GPS Series is a range of GNSS antennas designed for satellite applications, providing positioning, navigation, and timing capabilities.

Frequency	1575.42 MHz (GPS L1)
Antenna Type	Patch antenna with LNA
Gain	>25 dBic
Noise Figure	<1.5 dB
Interface	SMA connector

price on requestdatasheet

AAC Clyde Space

GNSS-701

The GNSS-701 is a space-qualified L-band patch antenna tuned to GPS frequency bands, suitable for MicroSats, SmallSats, and CubeSats.

Supported Constellations	GPS L1, GLONASS L1, Galileo E1
Position Accuracy (CEP)	<5 m (GPS L1)
Velocity Accuracy	<0.1 m/s
Time Accuracy	<100 ns
Channels	72 channels

price on requestdatasheet

AAC Clyde Space

iADCS200

The iADCS200 is an Attitude Determination and Control System (ADCS) designed for small satellites.

Pointing Accuracy	~1° (3σ)
Attitude Rate	<0.5°/s
Sensors	3-axis magnetometer, sun sensors, gyroscope
Actuators	3-axis magnetorquers
Interface	I2C / CAN

price on requestdatasheet

AAC Clyde Space

iADCS400

The iADCS400 is an integrated attitude determination and control system (ADCS) designed for small satellites, offering a complete solution for attitude control.

Pointing Accuracy	<0.1° (3σ) with star tracker
Attitude Rate	<0.05°/s
Sensors	3-axis magnetometer, sun sensors, gyroscope, star tracker interface
Actuators	3-axis reaction wheels + magnetorquers
Reaction Wheel Speed	Up to 6000 RPM

price on requestdatasheet

AAC Clyde Space

MAG-3

The MAG-3 is a high-precision magnetometer designed for autonomous satellite attitude control or scientific measurements.

Axes	3
Measurement Range	±100 µT
Resolution	0.1 nT
Accuracy	<2 nT (after calibration)
Noise Density	<0.1 nT/√Hz

price on requestdatasheet

AAC Clyde Space

MM200

The MM200 is a magnetorquer designed for small satellites, providing precise attitude control and reaction wheel desaturation.

Axes	3
Measurement Range	±100 µT
Resolution	0.05 nT
Noise Density	<0.05 nT/√Hz
Interface	I2C

price on requestdatasheet

AAC Clyde Space

MTQ800

The MTQ800 is a magnetorquer designed for attitude control in small satellites, offering a compact and efficient solution for detumbling and attitude stabilization.

Configuration	3-axis (X, Y, Z)
Dipole Moment (each axis)	0.2 A·m²
Max Current	0.5 A
Coil Resistance	~22 Ω
Interface	I2C / Analog PWM

price on requestdatasheet

AAC Clyde Space

PG400 Gyroscope

The PG400 is a flight-proven, high-performance standalone gyroscope designed for CubeSat and SmallSat attitude determination, offering low power consumption and a compact form fact

Gyroscope Range	-125 to 125 °/s
Zero rate offset	-1 to 1 °/s
Offset temperature drift	0.002 to 0.01 °/s/°C
Offset short term bias stability	1 °/h
Angular random walk	0.23 to 0.3 °/√h

price on requestdatasheet

AAC Clyde Space

RW222

The RW222 is a reaction wheel designed for small satellites, offering high reliability, adaptability, and accuracy for precise pointing.

Max Speed	±6000 RPM
Angular Momentum Storage	2.2 mNms
Max Torque	0.2 mNm
Motor Type	Brushless DC
Interface	I2C / CAN

price on requestdatasheet

AAC Clyde Space

RW400

The RW400 is a reaction wheel designed for small satellite missions, offering high reliability, adaptability, and accuracy for precise pointing.

Product Name	Trillian-1 (RW400)
Application	Small Satellite missions
Key Features	High reliability, adaptability, and accuracy

price on requestdatasheet

AAC Clyde Space

SS200

The SS200 is a compact and low-power sun sensor designed for attitude determination in CubeSats and small satellites.

Field of View	±60° (half-angle per axis)
Accuracy	<1° (1σ) in FOV
Update Rate	Up to 100 Hz
Interface	I2C / Analog
Supply Voltage	3.3 V

price on requestdatasheet

AAC Clyde Space

ST200

The ST200 is a star tracker designed for small satellites, providing attitude determination capabilities.

Attitude Accuracy (cross-boresight)	<10 arcsec (1σ)
Attitude Accuracy (roll)	<30 arcsec (1σ)
Update Rate	Up to 5 Hz
Acquisition Time	<5 s (initial), <1 s (tracking)
Field of View	15° x 15°

price on requestdatasheet

AAC Clyde Space

ST400

The ST400 is a high-performance star tracker designed for small satellite missions, offering precise attitude determination.

Attitude Accuracy (cross-boresight)	<3 arcsec (1σ)
Attitude Accuracy (roll)	<10 arcsec (1σ)
Update Rate	Up to 10 Hz
Acquisition Time	<2 s (initial), <0.2 s (tracking)
Field of View	10° x 10°

price on requestdatasheet

AAC Clyde Space

Trillian-1

High-performance reaction wheel for small satellites: 1.2 Nms momentum storage, 47.1 mNm max torque, 1.5 kg. Tested to NASA GEVS, flown since 2019.

Maximum Torque	47.1 mNm
Maximum Rotation Rate	6500 rpm
Total Momentum Storage	+/-1.2 Nms
Mass	1.5 kg
Peak Power	24 W

price on requestdatasheet

AAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from components to data analytics.

AAC SpaceQuest (AAC Clyde Space subsidiary)

ANT-GPS L-Band GPS Patch Antenna

Space-qualified L-band GPS patch antenna tuned to GPS frequency bands, ideal for MicroSats and SmallSats with recessed CubeSat mounting option.

Frequency Band	L-band (GPS L1/L2)
Type	Patch antenna
Target Platform	MicroSat, SmallSat (CubeSat recessed mounting)
Field of View	Hemispherical (GPS acquisition)
Applications	GPS/GNSS positioning, orbit determination

price on request

AAC SpaceQuest (AAC Clyde Space subsidiary)

GNSS-701 Satellite GNSS Receiver

Compact, high-performance satellite GNSS receiver — one of AAC SpaceQuest's bestselling components. Space-qualified for CubeSat and SmallSat orbit determination.

Type	GNSS receiver (GPS, multi-constellation)
Output	Position, velocity, time (PVT)
Target Platform	CubeSat, SmallSat
Design	Compact, low power
Heritage	Bestselling component, flight proven

price on request

AAC SpaceQuest (AAC Clyde Space subsidiary)

MAG-3 Three-Axis Satellite Magnetometer

Three-axis satellite magnetometer for reliable, accurate spacecraft attitude measurements, space-qualified for CubeSat and SmallSat ADCS.

Axes	3 (three-axis)
Measurement	Earth magnetic field vector
Applications	Attitude determination, B-dot detumbling, magnetorquer ADCS
Target Platform	CubeSat, SmallSat
Interface	Standard satellite bus interfaces

price on request

Accord Software & Systems designs and manufactures customized GPS/GNSS receivers for space applications and GPS/GNSS semiconductor chips for defense and commercial markets.

Accord

NAVLAN-IG3 Multi-Constellation GNSS Receiver

Indigenous Indian GNSS receiver with IRNSS L5, GPS, GLONASS, and GAGAN support — IP67 rated, 100 Mbps LAN interface, 1PPS output, Linux/Windows compatible.

Constellations	IRNSS L5, GPS L1, GLONASS L1, GAGAN L1
Ethernet	100 Mbps LAN, TCP/UDP
Serial	RS232/RS422, USB 2.0
Timing output	1 PPS
Protocol	NMEA 0183 Rev 4.10

price on request

Accord

NGS-N90 GNSS Network Time Server

Rack-mount GNSS time server with <20 ns timing accuracy, NTP v3/v4 and PTP IEEE 1588v2 support for 5000+ clients, supporting GPS, GLONASS, and IRNSS dual-frequency.

Timing accuracy	< 20 ns RMS (GPS)
PTP timestamp resolution	8 ns
Receiver channels	55
Constellations	GPS, SBAS (GAGAN), GLONASS, IRNSS (L5/S)
Protocols	NTP v3/v4, PTP IEEE 1588v2

price on request

Redwire is an integrated aerospace and defense company providing advanced technologies for space infrastructure, autonomous systems, and multi-domain operations to government agencies and defense cont

Adcole Space (Redwire)

Coarse Sun Sensor (Cosine Type)

A single-detector analog sun sensor using the cosine principle for solar array pointing, sun acquisition, and fail-safe recovery. Over 1,000 units deployed since the 1960s across h

Sensor Type	Analog cosine-response photodiode
Axes	1 (single axis per detector)
Configuration	Cosine type (single detector)
Field of View	Hemispherical (custom baffle options available)
Output	Analog current/voltage proportional to cos(angle)

price on requestdatasheet

Adcole Space (Redwire)

Coarse Sun Sensor (CSS) Pyramid

A two-axis analog sun sensor assembly containing four cosine-response detectors in a pyramid arrangement for full-hemisphere sun detection. Used for solar array pointing, sun acqui

Sensor Type	Analog cosine-response photodiode (×4)
Axes	2 (two-axis measurement)
Configuration	Pyramid (4-detector assembly)
Dry Mass	0.13 kg
Average Power	N/A (passive optical detection)

price on requestdatasheet

Adcole Space (Redwire)

Digital Sun Sensor (±32°)

A two-axis digital sun sensor with ±32° field of view offering higher accuracy than the ±64° variant. Radiation-hardened to 100 krad (Si) with Hi-Rel components for GEO and deep-sp

Field of View	±32°
Axes	2 (per optical head)
Output	Serial digital — two 10-bit words + sun presence bit
Radiation Hardness	100 krad (Si)
Components	Hi-Rel qualified

price on request

Adcole Space (Redwire)

Digital Sun Sensor (±64°)

A two-axis digital sun sensor with ±64° field of view providing medium-accuracy attitude determination. Up to 8 optical heads per electronics unit with proven deep-space flight her

Field of View	±64°
Axes	2 (per optical head)
Optical Heads per Electronics Unit	1–8 (configurable)
Output	Serial digital data stream (sun angle + sun presence bit)
Dry Mass	1.3 kg (electronics unit + 1 head)

price on requestdatasheet

Adcole Space (Redwire)

Fine Spinning Sun Sensor (±64°)

A high-accuracy spinning spacecraft sun sensor with redundant optical heads and electronics delivering better performance than the Miniature variant, for sun acquisition and attitu

Field of View	±64°
Dry Mass	0.71 kg
Average Power	0.4 W
Architecture	Redundant — 1 optical head per electronics channel
Application	Spinning spacecraft attitude determination, sun acquisition, fail-safe recovery

price on requestdatasheet

Adcole Space (Redwire)

Fine Sun Sensor

A high-precision sun sensor for attitude control applications requiring sub-arcminute accuracy and millidegree angular resolution. Available in single or dual-axis configurations a

Accuracy	Sub-arcminute
Resolution	Millidegree
Axes	1 or 2 (configurable)
Field of View	Custom (per mission requirement)
Heritage	Yes

price on requestdatasheet

Adcole Space (Redwire)

MAI-400 ADACS

The MAI-400 ADACS is a 1/2U Attitude Determination and Control System for small satellites, featuring reaction wheels, magnetometers, Earth Horizon Sensors, and torque rods for sta

Form Factor	1/2U
Components	3 reaction wheels, 3-axis magnetometer, 2-camera Earth Horizon Sensor (EHS), 3 torque rods
Compatibility	CubeSats
Placement	Bottom or top of CubeSat stack
Features	Cable channels for customer cable “Free-Arounds”

price on request

Adcole Space (Redwire)

MAI-400 Control Board

An attitude determination and control board incorporating four microcontrollers, MEMS accelerometer and gyroscope, and reaction wheel/electromagnet drive circuitry, compatible with

Board size	8.6cm x 8.8cm
Microcontrollers	Four (one ADACS processor, three reaction wheel control)
Accelerometer	3-axis MEMS accelerometer
Gyroscope	3-axis MEMS gyroscope
Drive circuitry	3 sets of Reaction Wheel and Electromagnet drive circuitry

$17 150 – $27 150

Adcole Space (Redwire)

MAI-400 Reaction Wheel

The MAI-400 reaction wheel is a standalone unit for CubeSats and NanoSat missions, featuring integrated motor driver electronics with an ARM Cortex CPU.

Availability

90 days

price on request

Adcole Space (Redwire)

MAI-KE Sun Sensor

The MAI-KE Sun Sensor is an analog sun sensor designed for spacecraft missions, providing an output voltage from 0 to 250mV.

Manufacturer	MAI
Lead time	90 days

price on request

Adcole Space (Redwire)

MAI-SES IR Earth Sensor

The MAI-SES is a miniature Static Earth Sensor designed for CubeSats, NanoSats, and larger spacecraft in Low Earth Orbit, measuring the dip angle with respect to the horizon using

Manufacturer	MAI
Lead time	90 days

price on request

Adcole Space (Redwire)

MAI-SS Space Sextant

The MAI-SS Star Tracker is low in cost and intended for CubeSat and NanoSat missions. The unit is completely self-contained and features lost in space star identification. Just…

Manufacturer

MAI

€28 434

Adcole Space (Redwire)

Miniature Spinning Sun Sensor

A compact sun sensor for spinning spacecraft providing sun aspect angle and sun crossing pulses for spin rate and spin axis orientation determination, with ±87.5° FOV and 0.25 kg m

Field of View	±87.5°
Dry Mass	0.25 kg
Average Power	0.5 W
Measurements	Sun aspect angle, sun crossing pulses
Application	Spinning spacecraft attitude determination

price on requestdatasheet

Adcole Space (Redwire)

SpectraTRAC Star Tracker

A miniature autonomous star tracker for CubeSat and NanoSat missions delivering 10 arcsecond quaternion accuracy at 4 Hz update rate, weighing only 475 grams with Lost-in-Space sta

Attitude Accuracy	10 arcsec (quaternion)
Output Rate	4 Hz
Maximum Tracking Rate	>2°/sec
Solution Availability	96.4%
Mass (with baffle)	475 g

price on requestdatasheet

Adcole Space (Redwire)

Sun Sensor Stimulator System

Ground support equipment using infrared LEDs to optically stimulate Adcole sun sensor cells for functional verification, aliveness testing, and flight harness checkout during space

Stimulus Type	Infrared LED optical illumination
Function	Sun sensor functional verification, aliveness testing, harness checkout
Control Interface	Front panel controls and/or computer input
Input Power	100–240 VAC, 50/60 Hz
Compatible Sensors	Adcole coarse and fine sun sensor families

price on requestdatasheet

Lithuanian CubeSat attitude control R&D company; spin-off of Kaunas University of Technology; miniaturised ADCS hardware for small satellite missions.

adpos

CubeSat Attitude Control System

Nano-satellite attitude control system in 1-DoF and 3-DoF configurations for CubeSat platforms, developed by ADPOS with trial models validated for primary experiments.

Degrees of freedom	1-DoF and 3-DoF configurations
Target platform	CubeSat / nano-satellites
Development stage	Trial models completed
Scalability	Extendable to micro-satellite class

price on request

Airbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration.

Airbus Defence and Space

Agile Actuators (CMG 15-45S, 40-60S, 75-75S)

Airbus offers a range of Control Moment Gyroscopes (CMGs) for satellites, providing precise agility and high reliability with torque outputs up to 75Nm.

Satellite mass range	500 kg to 3 tonnes
Torque output	up to 75Nm
Flight heritage	Over 1 million cumulative operational hours in orbit without failures
Operational duration	Over a decade

price on requestdatasheet

Airbus Defence and Space

AOCS & GNC Sensors

Airbus offers a comprehensive range of avionics sensors for precise attitude control and navigation in space, including Astrix fibre-optic gyroscopes, Jena-Optronik star sensors, a

ASTRIX 200 bias stability	<0.0005°/h
ASTRIX 120 bias stability	<0.01°/h, startup <3s
Interfaces	1553B, RS422
Mission life	15+ years continuous operation

price on requestdatasheet

Airbus Defence and Space

AOCS/GNC Sensors

A range of Airbus attitude and orbit control sensors comprising Astrix fibre-optic gyroscopes, Jena-Optronik star sensors, and BASS bi-axis sun sensors for satellite and spacecraft

Astrix bias stability	as low as 0.0005°/h
Astrix mission lifetime	exceeding 15 years
BASS field of view	±90°
BASS mass	low mass
BASS thermal resistance	high thermal resistance

price on requestdatasheet

Airbus Defence and Space

ASTRIX 1090 Inertial Measurement / Accelerometer Unit

Three-axis fibre-optic inertial unit from the ASTRIX 1000 series offering low angular random walk and optional accelerometer channels for navigation.

Angular random walk	<0.005°/√h
Bias stability	<0.01°/h
Configuration	Optional accelerometer channels for full inertial navigation
Flight heritage	3+ million flight hours

price on requestdatasheet

Airbus Defence and Space

Control Moment Gyroscopes (CMG 15-45S / 40-60S / 75-75S)

A range of compact, high-torque Control Moment Gyroscopes from Airbus for precise and agile satellite attitude control, covering satellites from 500 kg to 3 tonnes.

Models	CMG 15-45S, CMG 40-60S, CMG 75-75S
Applicable satellite mass range	500 kg to 3 tonnes
Torque output	Up to 75 Nm
Design features	Patented designs, integrated vibration dampers
Cumulative in-orbit operational hours	Over 1 million hours, without failures

price on requestdatasheet

UK-based nanosatellite kit company making space accessible through open-source 1U CubeSat education kits.

AmbaSat

AmbaSat-1 Sensor 08

The AmbaSat-1 Sensor 08 pack includes a TESEO-LIV3R GNSS receiver module and an AmbaSat-1 Daughterboard with all necessary components.

Module Dimensions	9.7x10.1 mm
Supported GNSS	GPS, Glonass, BeiDou, QZSS

price on request

French manufacturer of flight-proven space antennas, software-defined radio platforms, and RF payload technologies for satellite and launcher missions, with heritage on 200+ missions.

Anywaves

GNSS Antenna for Small Satellites

Miniaturized multi-constellation GNSS patch antenna for GPS, Galileo, GLONASS, and BeiDou reception on orbit.

Frequency	L1/E1 (1575.42 MHz)
Gain	≥3 dBic
Mass	<30 g
Operating temperature	-40 to +85 °C
Polarization	RHCP

price on request

Arcsec designs and manufactures star trackers and reaction wheels, with over 100 systems sold and 5 years of flight heritage.

arcsec

Sagitta Star Tracker

The Sagitta star tracker is arcsec’s standard, fully autonomous star tracker designed to fit in a CubeSat. It features an integrated baffle to reduce stray light effects and

Cross-boresight accuracy	2" (1σ)
Along-boresight accuracy	10" (1σ)
Dimensions	44 x 50 x 95 mm
Power	1500 mW
Supply voltage	5 V

price on request

arcsec

Scorpio Star Tracker

The Scorpio star tracker provides arc second range pointing accuracy for SmallSats and larger satellites, featuring custom algorithms for accuracy, robustness, and low computationa

Cross-boresight accuracy	2" (1σ)
Around-boresight accuracy	10" (1σ)
Dimensions	72 x 72 x 162 mm
Power	2000 mW
Supply voltage	5 V

price on requestdatasheet

arcsec

Twinkle Star Tracker

The Twinkle Star Tracker provides arc second range pointing accuracy for CubeSats and large satellites, featuring custom algorithms optimized for accuracy, robustness, and low comp

Cross-boresight accuracy	3" (1σ)
Around-boresight accuracy	30" (1σ)
Dimensions	20 x 20 x 40 mm
Power	1000 mW
Supply voltage	5 V

price on requestdatasheet

arcsec

Zyra Reaction Wheel

The Zyra reaction wheel is a compact, low microvibration reaction wheel designed for CubeSats up to 12U, featuring custom drive electronics and internal speed control.

Momentum Capacity	27.5 mNms
Torque	1.5 mNm
Dimensions	40 × 40 × 24.5 mm
Supply Voltage	5–12 V
Communication Interface	RS485

price on requestdatasheet

ASPINA is the corporate brand of Shinano Kenshi Co., Ltd., a Japanese precision technology group manufacturing motors, actuators, blowers, and electronic components for space, medical, and industrial applications.

ASPINA

ASPINA Reaction Wheels for Small Space Satellites

ASPINA offers a lineup of reaction wheels (RWs) designed for small satellite constellations in Low Earth Orbit (LEO), catering to CubeSats and satellites ranging from 100kg to 500k

Item	Developing specification
Model	ARW-3m
TRL	8
Heritage	1st units launched: Jan 2025
Satellite mass	CubeSat

price on request

ASPINA

Reaction wheel

ASPINA offers a range of reaction wheels designed for satellite attitude control, featuring competitive pricing, high production capacity, low disturbance, light weight, and high p

Item	Developing specification
Model	ARW-3m
TRL	8
Heritage	1st units launched: Jan 2025
Satellite mass	CubeSat

price on request

ASTER Labs (Advanced Space TEchnology Research) is a US space technology research laboratory developing spacecraft navigation tools, deep space navigation algorithms, CubeSat systems, and aerospace engineering software.

Azimut Space GmbH is a Berlin-based space engineering SME with 15+ years of experience in thermo-mechanical engineering, developing thermal control systems, payloads, scientific instruments, and ground support equipment for satellite, instr

Azimut Space

Navigation and Attitude Pointing Systems

Azimut Space's precision azimuth and elevation pointing systems and navigation equipment for satellite tracking antennas, ground stations, and airborne surveillance platforms.

Products	Az-El antenna positioners, gyro-stabilized platforms, pointing control systems
Pointing Accuracy	Arc-minute class (antenna tracking)
Encoder Resolution	19–23 bit angular (high-resolution servo systems)
Mobile Platforms	Gyro-stabilized systems for vehicles, aircraft, ships
Applications	Satellite ground tracking, remote sensing, airborne surveillance

price on request

Azista BST Aerospace is an Indo-German joint venture that mass manufactures small satellites (50-200kg) and provides end-to-end solutions for mega-constellations.

Azista BST Aerospace

RWA05 Reaction Wheel Assembly

Reaction wheel assembly for small satellites with integrated fibre-optic gyro, by Azista BST Aerospace.

Type	Reaction wheel assembly with integrated fibre-optic gyro
Application	Attitude control of small satellites
Product line	Azista BST subsystems (BAT-110, PCU-110, PPDH-110, PLSU, RWA05)

price on request

Chinese navigation technology group providing BeiDou and GNSS products, modules, and satellite-based solutions.

Huali Chuangtong (华力创通, Hwacreate) is a Chinese satellite navigation and IoT technology company listed on the Shenzhen Stock Exchange, headquartered in Beijing, developing GNSS (GPS/BeiDou) navigation modules, IoT terminals, and satellite c

Beijing Huali Chuangtong Technology Co., Ltd.

EBike-Tbox Smart Electric Bicycle IoT Terminal

The EBike-Tbox V30 is an intelligent IoT terminal designed specifically for electric bicycles, compliant with the Electric Bicycle Safety Technical Standard (GB17761-2024). It supp

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HBD2023 Beidou-3 Short Message RF-Baseband SoC Chip

The HBD2023 is a Beidou-3 short message RF-baseband integrated SoC chip supporting reception of B1I, B1C, B2a, B2b, and B3 signals for positioning, velocity measurement, and timing

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HBD4200 Marine Beidou Positioning Terminal

The HBD4200 is a multifunctional marine communication terminal integrating Beidou RDSS short message, Beidou high-precision positioning, 5G, Wi-Fi, and public network connectivity.

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HBD4201 Inland Vessel Beidou Terminal

The HBD4201 Inland Vessel Terminal is designed for river navigation management. It consists of a human-machine interaction tablet and a communication base. The tablet incorporates

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HBP2012 Beidou-2 Navigation Baseband Chip

The HBP2012 is a fully proprietary navigation baseband chip capable of simultaneously receiving BDS, GPS, and GLONASS signals. It can capture and track Beidou precision ranging cod

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HBP2020 Beidou-3 Multi-Mode Multi-Frequency Navigation Baseband Chip

The HBP2020 is the latest multi-system multi-frequency satellite navigation baseband chip from Hwa Create. It supports BDS, GPS, GLONASS, Galileo, QZSS, and SBAS full-system full-f

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HTG001 High-Precision Baseband Chip

The HTG001 is a high-precision Beidou baseband chip supporting RNSS navigation signal reception, acquisition, tracking, and computation. It provides single-frequency, dual-frequenc

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HTY512S Beidou Star-Ground Fusion Positioning Module

The HTY512S is a Beidou star-ground fusion positioning module supporting B3I, B1I, and B1C frequency bands in an industry-standard 16mm × 12.2mm stamp-hole package. It supports dua

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HWA-BD-820 Beidou High-Precision Receiver

The HWA-BD-820 is a high-precision Beidou receiver with anti-multipath capability, designed for deformation monitoring applications. Technical features: – Auto power-on, anom

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HWA-BD-M200 Geodetic Beidou Receiver

The HWA-BD-M200 is a geodetic-grade Beidou receiver for precision monitoring applications. It holds MIIT single-Beidou certification and supports only BDS single-system positioning

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HWA-BDS-M820 Portable Beidou Short Message Terminal

The HWA-BDS-M820 is a self-developed portable Beidou short message terminal supporting simultaneous Beidou short message, single Beidou positioning, and Bluetooth connectivity. It

price on request

Beijing Huali Chuangtong Technology Co., Ltd.

HWA-CZ200 Beidou Vehicle High-Precision Terminal

The HWA-CZ200 is a compact Beidou vehicle-mounted high-precision positioning terminal supporting both Beidou-3 and Beidou-2 systems. It provides high-precision Beidou satellite pos

price on request

Berlin Space Technologies (BST) designs and mass manufactures small satellite systems and technologies, providing end-to-end solutions for space missions.

Berlin Space Technologies

FSSA-110

The FSSA-110 is a Fine Sun Sensor Assembly from Berlin Space Technologies that hosts up to three analogue fine sun sensors, providing sun vector data to the satellite's OBC.

Accuracy	5°
Update Rate	10Hz
Coverage	Hemispherical
Sun Sensor Interface	5x Analogue per sensor
Data Interface	RS422

price on requestdatasheet

Berlin Space Technologies

GPS-110

The GPS-110 by Berlin Space Technologies is a miniature GPS receiver featuring two separate internal GPS receiver units and flight heritage since 2023.

Position Accuracy	< 10 m
Velocity Accuracy	0.1 m/s
Time to first fix	40s (cold start)
Power Consumption	3W
Data Interface	RS422

price on requestdatasheet

Berlin Space Technologies

RWA-05

The RWA05 by Berlin Space Technologies is a reaction wheel for small satellites, offering high precision and an optional integrated fibre optical gyro.

Angular Momentum Storage	5 arcsec
Torque (net)	14mNm
Typical Speed	5000rpm
Speed Control Accuracy	+/- 2rpm
Data Interface	RS422

price on requestdatasheet

Berlin Space Technologies

ST200

The ST200 is a miniaturized, autonomous star tracker designed for CubeSats and nano-satellites, providing a full attitude solution.

Accuracy	10 arcsec
Update Rate	5Hz
Limiting Magnitude	6.0
Sun Exclusion Angle	40°
Data Interface	UART (TTL), RS422 (optional)

price on requestdatasheet

Berlin Space Technologies

ST400

The ST400 is a high-precision star tracker developed in collaboration with AAC Hyperion, providing a full and autonomous attitude solution for demanding small satellite missions.

Accuracy	5 arcsec
Update Rate	5Hz
Limiting Magnitude	6.0
Sun Exclusion Angle	40°
Data Interface	UART (TTL), RS422 (optional)

price on requestdatasheet

Leading provider of small satellite buses, systems, and components for commercial, civil, and government space missions, a Raytheon (RTX) business.

Blue Canyon Technologies

Blue Canyon Technologies nano star tracker (NST)

The Blue Canyon Technologies nano star tracker (NST) is a flight-proven, high-performing, and reliable star tracker designed for spacecraft platforms, offering a low SWaP-C solutio

1P8S	1 string × 8 Li-ion cells in series
2P8S	2 strings × 8 Li-ion cells; ~2× energy of 1P8S
IP8S	Integrated pack variant
Chemistry	Li-ion
Compatible buses	BCT XB3, XB6, XB12, XB16 (XB1 avionics stack)

price on request

Blue Canyon Technologies

Control Moment Gyroscopes

Blue Canyon Technologies' Control Moment Gyroscopes (CMGs) offer significantly higher torque and lower power consumption compared to traditional reaction wheels, providing enhanced

CMG-8 Momentum	8 Nms
CMG-8 Torque	8 Nm
CMG-8 Mass	< 13 kg
CMG-12 Momentum	12 Nms
CMG-12 Torque	12 Nm

price on requestdatasheet

Blue Canyon Technologies

Nano Star Tracker (NST)

Blue Canyon Technologies' flight-proven nano star tracker is a low SWaP-C, turnkey starlight-in/quaternion-out attitude sensor for standalone missions and constellations.

Environmental qualification	Beyond GEVS level environments
Interface	Starlight-in, quaternion-out (turnkey)
Tracking sensitivity	Down to 7.5 magnitude
On-board star catalog	More than 20,000 stars

price on request

Blue Canyon Technologies

Nano Star Trackers

A family of low SWaP-C nano star trackers from Blue Canyon Technologies offering lost-in-space star identification across three form factors with proven flight heritage.

Standard NST - Mass	.35 kg
Standard NST - Dimensions	10 x 5 x 5.5 cm
Standard NST - Accuracy Cross-Boresight	6 arcsec
Standard NST - Accuracy About-Boresight	40 arcsec
Mid-Extension NST - Mass	.45 kg

price on request

Blue Canyon Technologies

Nano Star Trackers (NST)

Blue Canyon Technologies' Nano Star Trackers (NST) are low SWaP-C attitude sensors offering lost-in-space star identification with flight-proven heritage.

Standard NST - Mass	0.35 kg
Standard NST - Dimensions	10 x 5 x 5.5 cm
Standard NST - Accuracy Cross-Boresight	6 arcsec
Standard NST - Accuracy About-Boresight	40 arcsec
Mid-Extension NST - Mass	0.45 kg

price on request

Blue Canyon Technologies

Reaction Wheels

Blue Canyon Technologies offers a line of low-jitter reaction wheels ranging from 0.015 Nms to 16.0 Nms of momentum, designed for long life and vibration isolation.

RWp015 Max Momentum	0.015 Nms
RWp015 Max Torque	0.004 Nm
RWp015 Mass	0.13 kg
RWp050 Max Momentum	0.050 Nms
RWp050 Max Torque	0.007 Nm

price on requestdatasheet

Blue Canyon Technologies

RW Series Reaction Wheels

Blue Canyon Technologies’ RW (Reaction Wheel) series is one of the most flight-proven lines of miniaturized reaction wheels available for small spacecraft. The family scales

RW1	Smallest variant, 1U-3U CubeSat class
RW2 / RW2-HT	2U-6U class; HT = High-Temperature qualified variant
RW4 / RW4-HT	4U-6U class
RW8 / RW8-HT	6U-12U class; used in XB6/XB12
RW16 / RW16-HT	Largest variant for Saturn-400 and 16U+ platforms

price on request

Blue Canyon Technologies

RWP Series Reaction Wheels

The BCT RWP (Reaction Wheel Precision) series addresses the momentum and torque storage needs of microsatellite platforms above the 6U CubeSat class. The four variants — RWP015, RW

RWP015	Smallest RWP variant; microsatellite class
RWP050	Mid-range stored momentum
RWP100	Suitable for Venus/Saturn-class platforms
RWP500	Largest stored momentum; Saturn-400 and larger buses
Qualification	Qualified beyond GEVS-level environments

price on request

Blue Canyon Technologies

XACT

The XACT is an integrated attitude control solution for CubeSats, providing high-accuracy pointing capabilities for various missions.

XACT-15 Mass	.89 kg
XACT-15 Dimensions	10 x 10 x 5 cm (0.5U)
XACT-15 Supply Voltage	12 V
XACT-50 Mass	1.23 kg
XACT-50 Dimensions	10 x 10 x 7.54 cm (0.75U)

price on requestdatasheet

Swedish green propulsion pioneer; HPGP / LMP-103S thrusters using ADN propellant with 12% higher Isp than hydrazine; Bradford ENOVIA group.

Bradford Space

Bradford Coarse Sun Sensor (CSS)

Internally-redundant coarse sun sensor with full-sky 180×180° FOV, ±2° accuracy, 215 g, dual 9-pin D-sub interface, >100 kRad TID.

FOV	180 × 180°
Accuracy	±2° (3σ) at BoL
Resolution	< 0.1°
Noise Equivalent Angle	Negligible
Mass	215 g

price on requestdatasheet

Bradford Space

Bradford Cosine Sun Sensor (CoSS)

Compact 25 g cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 0 W passive, >100 kRad TID, 30×30×14 mm.

FOV	160 × 160°
Accuracy	±3° (3σ) OBC-limited
Resolution	< 0.1°
Noise Equivalent Angle	< 0.1° (3σ)
Mass	25 g

price on requestdatasheet

Bradford Space

Bradford Fine Sun Sensor (FSS)

High-accuracy fine sun sensor with ±0.3° accuracy (3σ), 128×128° FOV, 375 g, >100 kRad TID tolerance for demanding missions.

FOV	128 × 128°
Accuracy	±0.3° (3σ) across mission lifetime
Resolution	< 0.03°
Noise Equivalent Angle	< 0.05° (3σ)
Mass	375 g

price on requestdatasheet

Bradford Space

Bradford Mini Fine Sun Sensor (Mini FSS)

Ultra-compact 50 g sun sensor with ±0.2° accuracy (3σ), 128×128° FOV, 0 W passive operation, 50×46×17 mm.

FOV	128 × 128°
Accuracy	±0.2° (3σ) with LUT on OBC
Resolution	< 0.03°
Noise Equivalent Angle	< 0.005° (3σ)
Mass	50 g

price on requestdatasheet

Bradford Space

Bradford Redundant Cosine Sun Sensor (COSS-R)

Self-redundant cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 15 g ultralight, 0 W passive, >100 kRad TID.

FOV	160 × 160°
Accuracy	±3° (3σ) OBC-limited
Resolution	< 0.1°
Noise Equivalent Angle	Negligible
Mass	15 g

price on requestdatasheet

Bradford Space

Coarse Sun Sensor (CSS)

Rugged self-redundant sun sensor delivering coarse solar position data for safe-mode and coarse maneuvering.

Field of View	Hemispherical
Redundancy	Self-redundant
In Production Since	1975

price on request

Bradford Space

Cosine Sun Sensor Redundant (COSS-R)

Self-redundant cosine-response sun sensor delivering reliable wide-angle solar position data for safe-mode operations.

Angular Response	Cosine
Redundancy	Self-redundant

price on request

Bradford Space

Fine Sun Sensor (FSS)

Analogue quadrant-detector sun sensor providing precise two-axis solar aspect angle for yaw steering and earth-pointing missions.

Detector Type	Analogue quadrant detector
Axes	2
Output	4 quadrant voltages + sun presence voltage

price on request

Bradford Space

Mini Fine Sun Sensor (Mini-FSS)

Compact, lightweight version of the Fine Sun Sensor for small satellites and CubeSats requiring precise sun-vector data.

Detector Type	Analogue quadrant detector
Axes	2
Form Factor	Compact / lightweight

price on request

Bradford Space

W18 Reaction Wheel

Compact reaction wheel assembly with analogue or digital interface, proven zero-crossing and low-RPM performance.

Interface	Analogue or Digital
Flight Heritage	SOHO, RadarSat, Seastar, Olympus, Integral, XMM, Rosetta, Aeolus, BepiColombo

price on requestdatasheet

Bradford Space

W18E Reaction Wheel

Extended-capacity variant of the W18 reaction wheel assembly for small and medium satellite attitude control.

Interface	Analogue or Digital
Product Line	W-series Reaction Wheel Unit

price on requestdatasheet

Bradford Space

W18ES Reaction Wheel

High-capacity W18-series reaction wheel variant offering extended momentum storage for demanding pointing missions.

Interface	Analogue or Digital
Product Line	W-series Reaction Wheel Unit

price on requestdatasheet

Bradford Space

W45 Reaction Wheel

Larger-class reaction wheel assembly from Bradford Space's W-series for medium and large satellite platforms.

Interface	Analogue or Digital
Flight Heritage	SOHO, RadarSat, Seastar, Olympus, Integral, XMM, Rosetta, Aeolus, BepiColombo

price on requestdatasheet

Bradford Space

W45E Reaction Wheel

Extended-capacity W45-series reaction wheel for large satellite platforms requiring maximum momentum storage.

Interface	Analogue or Digital
Product Line	W-series Reaction Wheel Unit

price on requestdatasheet

Canon Electronics Inc. develops and manufactures small artificial satellites and their components, alongside a diverse range of precision machinery, electronic equipment, and optical products.

Canon Electronics - Space

TMFセンサー

TMF sensors are high-frequency driven magnetic sensors developed by Canon Electronics, utilizing proprietary magnetic thin films for various magnetic detection needs. They come in

price on request

CHC Navigation provides geospatial, machine control, navigation, and agriculture solutions utilizing GNSS, LiDAR, UAV, USV, and INS technologies.

CHC Navigation / Huace Daohang

CHCNAV i93

The i93 is CHC Navigation's flagship IMU-RTK GNSS smart antenna, combining a 1892-channel multi-constellation receiver with an auto-tilt IMU and dual cameras for visual surveying a

GNSS constellations	GPS, GLONASS, Galileo, BeiDou, QZSS, SBAS, NavIC/IRNSS
Receiver channels	1892-channel
RTK accuracy (horizontal)	0.8 cm
RTK accuracy (vertical)	1.5 cm
PointSky PPP accuracy	2.5 cm horizontal / 5 cm vertical

price on request

CHC Navigation / Huace Daohang

High-Precision GNSS Survey Receivers

CHC Navigation's professional-grade dual/triple-frequency RTK GNSS receivers and surveying instruments supporting BeiDou, GPS, Galileo, and GLONASS for centimeter-level positioning

Technology	Triple-frequency RTK GNSS (BeiDou-3, GPS, GLONASS, Galileo, QZSS, NavIC)
Accuracy	±8 mm horizontal + 1 ppm RTK (typical)
Products	RTK rover/base receivers, UAV GNSS, marine receivers, machine control
Export Markets	140+ countries
Certifications	ISO 9001, CE

price on request

Collins Aerospace, an RTX company, delivers advanced avionics, communication systems, and space technology solutions to commercial aviation, defense, and space customers worldwide.

Collins Aerospace

High Motor Torque Momentum and Reaction Wheels

Collins Aerospace offers Teldix space wheels with integrated wheel drive electronics, providing angular momentum storage from 0.04 to 68 Nms for spacecraft weighing 30 kg to 7,000

Angular momentum storage capacity	0.04 to 68 Nms
Integrated wheel drive electronics	14 to 68 Nms
Accommodates spacecraft weighing	30 kg to 7,000 kg
Suitable for satellites weighing	1,500 to 5,000 kg
Combined in-orbit operational time	More than 7,300 years

price on request

Collins Aerospace

RSI 4-75/60 Momentum and Reaction Wheel

Compact TELDIX momentum/reaction wheel with integrated wheel drive electronics for small satellite attitude control, 0.04-4 Nms class.

Mass	3.7 kg
Power	20.0 W average
Interface	Form factor: SmallSat
Flight heritage	Part of TELDIX wheel family with 40+ years heritage, 7,300+ cumulative in-orbit years
TRL	9 (flight-proven)

price on requestdatasheet

Collins Aerospace

Teldix High Motor Torque Momentum and Reaction Wheels

Collins Aerospace's Teldix space wheels are high motor torque momentum and reaction wheels with integrated wheel drive electronics, used in spacecraft attitude control systems.

Wheel drive electronics integration	14 to 68 Nms
Angular momentum storage capacity	0.04 to 68 Nms
Supported spacecraft mass range	30 kg to 7,000 kg
High motor torque variant satellite mass range	1,500 to 5,000 kg
Lifetime design	More than 15 years

price on requestdatasheet

Collins Aerospace

TELDIX RSI 12 Momentum and Reaction Wheels

Compact TELDIX momentum and reaction wheels with integrated wheel drive electronics at 4 to 12 Nms, for satellites weighing 200 to 1,000 kg.

Momentum range	4 to 12 Nms
WDE	Integrated Wheel Drive Electronics
Target platform	Satellites 200–1,000 kg
Design lifetime	> 15 years
Heritage	7,300+ years cumulative in-orbit operational time

price on request

Collins Aerospace

TELDIX RSI 45 Momentum and Reaction Wheels

TELDIX momentum and reaction wheels with integrated WDE at 15 to 45 Nms and high torque capability, for satellites weighing 500 to 1,500 kg.

Momentum range	15 to 45 Nms
WDE	Integrated Wheel Drive Electronics
Target platform	Satellites 500–1,500 kg
Design lifetime	> 15 years
Heritage	7,300+ years cumulative in-orbit operational time

price on request

Collins Aerospace

TELDIX RSI 68 Momentum and Reaction Wheels

High-capacity TELDIX momentum and reaction wheels with internal WDE at 14 to 68 Nms, for large satellites weighing 1,500 to 5,000 kg.

Momentum range	14 to 68 Nms
WDE	Internal Wheel Drive Electronics
Target platform	Satellites 1,500–5,000 kg
Design lifetime	> 15 years
Heritage	7,300+ years cumulative in-orbit operational time

price on request

Collins Aerospace

TELDIX® Space Wheels

Collins Aerospace TELDIX® Space Wheels are a range of momentum and reaction wheels designed for reliable and durable attitude control in spacecraft and satellites.

Mass	7.6 kg
Power	20.0 W average
Interface	Form factor: SmallSat; External Wheel Drive Electronics (WDE), cascadeable
Flight heritage	Part of TELDIX wheel family, 2,900+ cumulative in-orbit years
TRL	9 (flight-proven)

price on request

Comat is a French aerospace equipment manufacturer, part of the Hemeria group, designing flight hardware and mechanisms for small satellites, telecommunications/observation payloads, and space exploration missions.

Comat

Small Sat Reaction Wheels

A range of plug-and-play, radiation-proof reaction wheels designed for small satellites from 10 kg to 1000 kg, offering long lifespan and safeguarded electronics.

Random	21 grms
Shock	1,000 g/2,000 Hz
Minimum Speed	Down to 2 rpm
Zero Crossing Tests	More than 100,000
Operational Life	10 years

price on request

South African manufacturer of space-proven, plug-and-play Attitude Determination and Control Systems (ADCS) for small satellites, with over a decade of flight heritage.

CubeSpace ADCS

Fine Sun Sensor – CubeSense Sun

CubeSense Sun is a high-accuracy CMOS-based fine sun sensor with a wide field of view (FOV). Optimized for low power consumption, it features a pre-calibrated distortion model,…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Infrared (IR) Earth Horizon Sensor

The CubeSense Earth is a compact and reliable infrared earth horizon sensor providing high-accuracy nadir determination for satellite control, especially in eclipse, without needin

Accuracy [*]	1° (roll and elevation) 3-sigma
Max slew rate [°/s]	14
Mass [g]	18
Dimensions [WxHxL] [mm]	35x24x20
Detection field of view [°] (Horizontal/vertical)	90/80

price on request

CubeSpace ADCS

Magnetometer (Compact & Deployable)

A robust 3-axis controlled magnetometer available in compact and deployable form factors, designed for satellite attitude determination and control systems.

Noise per channel [3-sigma] [nT]	50 (Magnetometer Deployable)
Noise per channel [3-sigma] [nT]	120 (Magnetometer Compact)
Linearity [full scale] [%]	0.6 (Magnetometer Deployable)
Linearity [full scale] [%]	0.6 (Magnetometer Compact)
Sensitivity [nT]	13 (Magnetometer Deployable)

price on request

CubeSpace ADCS

Magnetorquer Rods (CR0002-CR0020)

CubeSpace Magnetorquer Rods are space-proven magnetic torquers designed for satellite attitude control, featuring a compact design, robust mounting, and a range of magnetic moments

Max Voltage [V] (CR002)	5
Max Voltage [V] (CR003)	5
Max Voltage [V] (CR004)	5
Max Voltage [V] (CR005)	5
Max Voltage [V] (CR006)	5

price on request

CubeSpace ADCS

Reaction Wheel (CW40K) (4Nms)

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW0017

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW0057

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW0162

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW0500

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW10k (1 Nms)

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW1200 (0.12 Nms)

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW2500 (0.25 Nms)

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Reaction Wheel CW5000 (0.5 Nms)

CubeSpace (CS) offers a wide range of robust reaction wheels perfect for CubeSats and SmallSats. Our reaction wheel range is designed for precision performance, reliability, ease…

Manufacturer	CubeSpace
Lead Time	12 weeks

price on request

CubeSpace ADCS

Star Tracker – CubeStar

CubeStar is a medium-to-high accuracy miniature star tracker equipped with an external thread for the easy integration of a mission-specific baffle, allowing you to customize the…

Manufacturer	CubeSpace
Lead Time	16 weeks

price on request

CubeSpace ADCS

Turn-Key ADCS

CubeSpace's Turn-Key ADCS is a space-proven, plug-and-play attitude determination and control system for CubeSats and SmallSats, available in integrated (3-6U) and distributed (lar

Technology readiness level	TRL 9 (flight-proven)
Form factor	Integrated for 3U-6U CubeSats; distributed for larger SmallSats
Actuators	Reaction wheels (with optional integrated damping), magnetorquer rods
Sensors	Star trackers, fine/coarse sun sensors, earth horizon sensors, magnetometers, gyroscopes,
Mission modes	Detumbling, sun-spin, earth target tracking, TDI imaging, inter-satellite tracking

price on request

Spanish space engineering group (founded as Deimos Space, part of Elecnor 2001-2024) now operating as Indra Space, delivering end-to-end satellite platforms, avionics, ground segment, GNSS and space-surveillance solutions.

Deimos Space (Indra)

Navishield Anti-Jam / Anti-Spoofing GNSS Antenna

Next-generation CRPA antenna system protecting GNSS receivers against interference and spoofing.

Protected signals	Galileo PRS, Galileo OS, GPS
Function	Anti-jam / anti-spoofing CRPA antenna
Related receiver	G3Star multi-constellation receiver (supports Galileo HAS)
Programme heritage	25+ years on the European Galileo programme

price on request

Deimos Space (Indra)

READY ADCS (READY-6U / 16U / 100 / 200)

Turnkey attitude determination and control system family for CubeSats and small satellites in LEO.

Product family	READY-6U, READY-16U, READY-100, READY-200
Target platform class	CubeSats (6U/16U) through 100-200 kg smallsat buses
Orbit regime	LEO
Architecture	Modular, configurable, off-the-shelf

price on request

Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.

ElmSpace

FDA Fluid Dynamic Attitude Control System

Novel fluid-dynamic attitude control system using fluid mass transfer to generate spacecraft torques without moving mechanical parts.

Actuation principle	Fluid mass transfer (fluid-dynamic torque generation)
Application	Spacecraft attitude control actuation
Platform	Nanosatellites, small satellites
Manufacturer	ElmSpace (Germany)

price on request

ElmSpace

Fluid Dynamic Attitude Control System (FDA)

Passive fluid-dynamic attitude control system for CubeSat stabilization — no moving parts or propellant.

Type	Passive fluid-dynamic attitude control system
Moving parts	None
Propellant required	None
Stabilization method	Closed-loop fluid dynamics
Application	CubeSat and small satellite passive attitude stabilization

price on requestdatasheet

ElmSpace

G-200 Gyroscope

Compact gyroscope for CubeSat and small satellite attitude determination.

Type	Gyroscope (rate sensor)
Application	CubeSat and small satellite ADCS
Model	G-200

price on requestdatasheet

ElmSpace

G-510 Gyroscope

High-performance gyroscope for small satellite attitude rate measurement and ADCS integration.

Type	Gyroscope (rate sensor)
Model	G-510
Application	CubeSat and small satellite ADCS

price on requestdatasheet

ElmSpace

G500 Gyroscope

Compact gyroscope for spacecraft attitude determination in nanosatellite and small satellite missions.

Application	Spacecraft attitude determination (nanosatellites, small satellites)
Function	Angular rate measurement
Interface	Compatible with standard ADCS integration
Manufacturer	ElmSpace (Germany)

price on request

EREMS is a French SME founded in 1979, specializing in the design and realization of electronic equipment and software for high technology fields including Space.

EREMS

ARIETIS Gyro Unit

3-axis space-qualified, radiation-hardened gyroscope for satellite AOCS — medium-accuracy, low-noise, suited for LEO, MEO, and GEO missions.

Measurement axes	3-axis
Accuracy class	Medium accuracy
Noise	Very low noise across full bandwidth
Target missions	LEO Earth observation, MEO navigation, GEO telecom

price on request

EREMS

JANSPER Reaction Wheel Controller

Electronic controller for driving and monitoring satellite reaction wheels — acquires commands, monitors sensors, controls wheel motor for attitude control.

Function	Reaction wheel driving and monitoring
Scope	Full development, manufacturing, and qualification by EREMS

price on request

German manufacturer of reaction wheels, CubeSat picosatellite deployers, and AOCS components for small satellites, based in Berlin-Adlershof.

EXA (Astro-und Feinwerktechnik)

ASTROFEIN ACM Magnetometer

The ASTROFEIN ACM Magnetometer is a high-precision, space-qualified magnetometer designed for attitude control in small and larger satellites, offering an optimal balance of low ma

Range	±60 000 nT (up to 140 000 nT on request)
Resolution	100 pT/LSB
Noise	50 pT/ √Hz@60 000 nT
Linearity	0.025%
Mass	< 280 g

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

ASTROFEIN Gyro System AGS-1

The ASTROFEIN Gyro System AGS-1 is a tri-axial rotation measurement system designed for small satellites, offering temperature-compensated data and low power consumption.

Channels	3
Range (per channel)	± 40 °/s
Bias (per channel)	≤ 1 °/h
Noise (random walk per channel)	≤ 0.1 °/ √ h
Measurement frequency	200 Hz

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

MicroCMG

The MicroCMG is a Control Moment Gyroscope designed for small satellites, providing attitude control with high angular momentum and torque capabilities.

Angular momentum	8.0 Nms
Nominal rotation speed	3820rpm
Nomial torque	14.0 Nm
Mass	≤ 8.0 kg
Dimension	188 x 188 x 240 mm³

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW1

The RW1 is a reaction wheel designed for small satellites, featuring separate wheel drive electronics and available with two different rotating masses (Type A or Type B) to provide

Parameter	Type A
Angular momentum	5.8 E-4 Nms
Nominal rotation speed	8000 rpm
Maximum rotation Speed	≈ 16 380 rpm
Speed Resolution	0.25 rpm (1LSB)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW100

The RW100 is a reaction wheel for small satellites, optimized for constellation applications and based on the RW90 design.

Angular momentum	0.4 Nms @ nominal speed
Nominal rotation speed	6000 rpm
Nomial reaction torque	0.02 Nm Max. commandable deliverable output torque over the whole speed range
Supply voltage	18 to 34 V
Power consumption	≤ 2 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW150

The RW150 is a reaction wheel designed for small satellites, featuring integrated wheel drive electronics, various operation modes, and high torque and speed stability.

Angular momentum	1.0 Nms
Nominal rotation speed	6000 rpm
Nomial reaction torque	0.03 Nm
Supply voltage	18 to 34 V
Power consumption Stand by (motor off)	≤ 2 W

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW1500

The RW1500 is a reaction wheel currently under development, designed for satellite attitude control with an angular momentum of 25.0 Nms and a nominal rotation speed of 4000 rpm.

Angular momentum	25.0 Nms @ nominal speed
Nominal rotation speed	4000 rpm
Nomial reaction torque	0.2 Nm Max. commandable reaction torque
Supply voltage	22 to 37 V
Power consumption	≤ 2.5 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW25

The RW25 is a compact reaction wheel designed for nano-satellite applications, featuring integrated electronics for independent operation via a digital interface.

Angular momentum	30 mNms
Nominal rotation speed	5000 rpm
Nomial Torque (max. commandable)	2 mNm (more by design possible)
Communication	SPI preferred (CAN possible)
Supply voltage	5 V

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW250

The RW250 is a reaction wheel for small satellites, featuring integrated wheel drive electronics, various operation modes, and extensive housekeeping data.

Angular momentum	4.0 Nms @ nominal speed
Nominal rotation speed	5000 rpm
Nomial reaction torque	0.1 Nm Max. commandable deliverable output torque over the whole speed range
Supply voltage	23 to 34 V
Power consumption	≤ 2.5 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW3000

The RW3000 is a reaction wheel designed for satellite attitude control, currently under development. It offers an angular momentum of 50 Nms and a nominal reaction torque of 0.2 Nm

Angular momentum	50.0 Nms @ nominal speed
Nominal rotation speed	4000 rpm
Nomial reaction torque	0.2 Nm Max. commandable reaction torque
Supply voltage	22 to 37 V
Power consumption	≤ 2.5 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW35

The RW35 is a reaction wheel designed for small satellites, featuring integrated drive electronics, high torque and speed stability, and extensive housekeeping capabilities.

Angular momentum	0.1 Nms
Nominal rotation speed	5000 rpm
Nomial Torque (max. commandable)	0.005 Nm
Moment of inertia (rotating mass)	1.9 x 10-4 kgm2
Supply voltage	18 V - 34 V

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW6000

The RW6000 is a large reaction wheel currently under development by ASTROFEIN, designed for satellite attitude control with high angular momentum and reaction torque capabilities.

Angular momentum	100.0 Nms @ nominal speed
Nominal rotation speed	4200 rpm
Nomial reaction torque	0.2 Nm Max. commandable reaction torque
Supply voltage	23 to 34 V
Power consumption	≤ 5.0 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW800

The RW800 is a reaction wheel for satellites, currently under development with an engineering model available, designed for attitude control.

Angular momentum	12.0 Nms
Remark	@ nominal speed
Nominal rotation speed	3600 rpm
Nomial reaction torque	0.2 Nm
Remark	Max. commandable reaction torque

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RW90

The RW90 is a reaction wheel designed for small satellites, featuring integrated drive electronics, multiple operation modes, and high torque and speed stability.

Angular momentum	0.35 Nms @7800 rpm
Nominal rotation speed	6000 rpm
Nomial reaction torque	0.015 Nm Max. commandable deliverable output torque over the whole speed range
Power consumption	≤ 1.8 W Stand by (motor off)
Power consumption	≤ 2.7 W @ 3000 rpm

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reaction Wheel RWT250

The RWT250 is a reaction wheel designed for small satellites, featuring integrated wheel drive electronics, various operation modes, and extensive housekeeping data.

Angular momentum	4.0 Nms @ nominal speed
Nominal rotation speed	5000 rpm
Nomial reaction torque	0.3 Nm Max. commandable deliverable output torque over the whole speed range
Supply voltage	23 to 34 V
Power consumption	≤ 3.0 W Stand by (motor off)

price on requestdatasheet

EXA (Astro-und Feinwerktechnik)

Reation Wheel RWT150

The RWT150 is an upscaled reaction wheel for small satellites, currently under development, designed to provide attitude control with a nominal angular momentum of 1.0 Nms.

Angular momentum	1.0 Nms @ nominal speed
Nominal rotation speed	6000 rpm
Nomial reaction torque	0.1 Nm Max. commandable deliverable output torque over the whole speed range
Supply voltage	18 to 34 V
Power consumption	≤ 2.5 W Stand by (motor off)

price on requestdatasheet

Ecuadorian civilian space agency and manufacturer of high-energy-density batteries, deployable solar arrays and CubeSat platforms.

EXA (Ecuadorian Space Agency)

EXA MT01 Compact Magnetorquer

With only 7.5 grams and 3.2 millimeters thickness, the MT01 Compact Magnetorquer is a vacuum core magnetic coil designed fo ADCS control in cubesat mission from 1U to 3U that…

Manufacturer	EXA
Lead time	2 weeks

price on request

Flywheel Aerospace designs and manufactures modular robotics platforms and educational kits, serving universities, research labs, and startups in India with solutions for robotics, AI, and space techn

Flywheel Aerospace

Flywheel Aerospace Momentum Storage Systems

Indian company developing flywheel-based momentum and energy storage systems for satellite attitude control applications.

Technology	Flywheel momentum/energy storage
Application	Satellite attitude control
Country	India

price on request

Singapore-based spacecraft studio building mass-producible small satellite platforms and offering low-cost flight heritage and imagery intelligence services.

Galamad Aerospace

Magnetorquer

High-performance magnetic torquers designed for precise attitude control of CubeSats and SmallSats, featuring a high magnetic dipole moment to mass ratio and low power consumption.

Magnetic Dipole Moment to mass ratio	High
Power Consumption	<1W per Asqm
Design	Compact and Lightweight

price on request

Georgia Tech's Space Systems Design Laboratory (SSDL) develops small satellites and CubeSats for formation flying, precision ranging, and mission autonomy research.

Georgia Institute of Technology

Ranging and Nanosatellite Guidance Experiment (RANGE)

RANGE is a mission consisting of two 1.5U CubeSats designed to demonstrate improved absolute orbital position knowledge and inter-satellite distance measurement using laser ranging

Project Sponsor	Terra Bella (formerly Skybox) University Cubesat Partnership
Start Date	08/25/2015
Faculty Investigator	Dr. Brian Gunter
Project Status	Currently in orbit
Number of CubeSats	Two

price on request

Gimbal Space designs and manufactures custom attitude determination and control systems (ADCS), including integrated systems, for customers with GNC teams.

Gimbal Space

NOVA and SUPERNOVA Star Trackers

Low-cost, high-accuracy star trackers with optional baffle for stray-light rejection — NOVA and SUPERNOVA configurations for smallsat attitude determination.

Configurations	Low-cost and high-accuracy options
Accessories	Baffle available (stray-light rejection)

price on request

Gimbal Space

Reaction Wheels

Custom-configurable reaction wheels for spacecraft attitude control — reliable, affordable, readily-available ADCS hardware for smallsat missions.

Configuration	Custom solutions available
Sizes	Multiple sizes

price on request

Gimbal Space

Torque Rods

Custom magnetorquer rods for satellite attitude control, available in multiple sizes — reaction-wheel desaturation and fine attitude control for smallsats.

Configuration	Custom solutions available
Sizes	Multiple sizes

price on request

Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

Glavkosmos

Altitude Control System

An Altitude Control System (ACS) designed for spacecraft, providing orientation accuracy of 1 degree and stabilization accuracy of 30 deg. s/s, with communication via CAN and debug

Purpose	Used in spacecraft as a control system.
Year of release	2018
Guaranteed service life (years)	LEO - 1 year
Estimated production / delivery time (months)	12
Flight qualification of the product	No

price on request

Glavkosmos

Antenna AFU-NMSS M

An all-ceramic active GLONASS/GPS antenna module for wearable satellite navigation receivers, operating through space navigation systems.

Year of release	2013
Guaranteed service life (years)	3
Estimated production / delivery time (months)	3
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Antenna ASNB-1

The Antenna ASNB-1 is a microstrip active antenna module designed for GLONASS/GPS on-board dual-band navigation receivers, specifically for rocket technology applications.

Purpose	GLONASS / GPS on-board dual-band navigation receiver (rocket technology). Work through spa
Year of release	2012
Guaranteed service life (years)	3
Estimated production / delivery time (months)	3
Flight qualification of the product	No

price on request

Glavkosmos

Antenna ASNB-2

A microstrip active antenna module for onboard GPS/GLONASS/GALILEO/BEIDOU satellite navigation system (SNS) equipment.

Purpose	In GPS / GLONASS / GALLILEO / BEIDOU on-board goniometer equipment. Work through space nav
Year of release	2017
Guaranteed service life (years)	3
Estimated production / delivery time (months)	3
Flight qualification of the product	No

price on request

Glavkosmos

Antenna ASNK-1

A wearable, all-ceramic active antenna module for GLONASS/GPS navigation, designed to work with satellite navigation systems.

Purpose	GLONASS / GPS wearable receiver. Work through space navigation systems (SNS).
Year of release	2011
Guaranteed service life (years)	3
Estimated production / delivery time (months)	3
Flight qualification of the product	No

price on request

Glavkosmos

Antenna ASNP-2M

Microstrip active antenna module for personal GLONASS/GPS receivers, designed to work through satellite navigation systems (SNS).

Purpose	As part of a personal GLONASS / GPS receiver. Work through space navigation systems (SNS).
Year of release	2011
Guaranteed service life (years)	3
Estimated production / delivery time (months)	3
Flight qualification of the product	No

price on request

Glavkosmos

Antenna-feeder Device BASN

The Antenna-feeder Device BASN is designed to receive navigation signals from GLONASS and GPS satellites, featuring flight qualification and heritage on the Meteor-3M spacecraft.

Purpose	Designed to receive information from navigation signals from GLONASS and GPS satellites.
Year of release	2000
Guaranteed service life	7 years
Estimated production / delivery time	5 months
Flight qualification of the product	Yes

price on request

Glavkosmos

Backup Inertial Measuring Device

The Backup Inertial Measuring Device is a sealed monoblock unit designed to measure angular velocities in three axes, intended for future manned spacecraft.

Purpose	Measurement of angular velocities in three axes.
Year of release	2018
Guaranteed service life (years)	10
Flight qualification of the product	No
Brief history of flight qualification	The instrument is being developed for future manned spacecraft.

price on request

Glavkosmos

Compact Star Tracker

A compact star tracker designed for small spacecraft (nano- and micro-satellites) to determine their orientation by the star field.

Purpose	Orientation of spacecraft by the star field.
Year of release	2017
Guaranteed service life (years)	3 years in LEO (300-800 km)
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Electromagnet EM-IF-20

The Electromagnet EM-IF-20 is a core electromagnet designed for the stabilization equipment of spacecraft, featuring a harness and connector.

Purpose	Executive electromagnet of stabilization spacecraft equipment.
Year of release	2012
Guaranteed service life	12 years
Estimated production / delivery time	8 months
Flight qualification of the product	Da

price on request

Glavkosmos

Electromagnetic Unit (EMU) – Magnetic Torquer

The Electromagnetic Unit (EMU) is a magnetic torquer designed for spacecraft attitude control systems, creating a dipole magnetic moment proportional to the current flowing through

Year of release	2016
Guaranteed service life (years)	5
Estimated production / delivery time (months)	6
Flight qualification of the product	No
Brief history of flight qualification	Flight tests, normal operation.

price on request

Glavkosmos

Electromagnetic Unit (EMU) – Magnetic Torquer for Nanosatellites

The Electromagnetic Unit (EMU) is a magnetic torquer for nanosatellites, designed to create a dipole magnetic moment proportional to the current in its windings, used for attitude

Year of release	2019
Guaranteed service life	5 years
Estimated production / delivery time	3 months
Flight qualification of the product	Yes
Brief history of flight qualification	Ground experimental testing.

price on request

Glavkosmos

GNSS Receiver

A compact multi-constellation GNSS navigation receiver module that computes real-time coordinates, speed, and precise time, and exchanges data with external equipment via serial in

Purpose	Navigation and communications equipment
Year of release	2017
Guaranteed service life (years)	3
Estimated production / delivery time (months)	7
Flight qualification of the product	No

price on request

Glavkosmos

GNSS Receiver in a Secure Enclosure

GPS+GLONASS L1 navigation receiver in secure case (16 ch, 9 m CEP, 2×RS-232, 71×51×12 mm, 50 g, -40 to +85 °C, 0.65 W). For mission-critical applications.

Purpose	Mission-critical navigation systems
Year of release	2007
Guaranteed service life, years	3
Estimated production/delivery time	6 months
Flight qualification	No

price on request

Glavkosmos

Gyroscope Sensor for Measuring Angular Velocity Vector Projections 1

A redundant, free-form gyroscopic angular velocity vector meter designed for spacecraft orientation and stabilization control systems, measuring angular increments on four sensitiv

Purpose	Measurement of angular increments (rate integral) on sensitive axes of four measurement ch
Year of release	1996
Guaranteed service life	15 years
Estimated production / delivery time	18 months
Flight qualification of the product	Yes

price on request

Glavkosmos

Gyroscope Sensor for Measuring Angular Velocity Vector Projections 2

A redundant, free-form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control systems, featuring four fiber-optic gyroscopes and four pendulu

Purpose	Measurement of angular increments (rate integral) on sensitive axes of four measurement ch
Year of release	2016
Guaranteed service life (years)	15
Estimated production / delivery time (months)	18
Flight qualification of the product	Yes

price on request

Glavkosmos

Gyroscope Sensor for Measuring Angular Velocity Vector Projections 3

A three-channel fiber-optic gyroscope sensor designed to measure angular velocity vector projections and transmit this data to a spacecraft's control system.

Purpose	Measurement of angular increments (rate integral) on sensitive axes of three measurement c
Year of release	2011
Guaranteed service life	10 years
Flight qualification of the product	Yes
Brief history of flight qualification	Produced and shipped to the Customer more than 20 ea. The instruments passed flight tests

price on request

Glavkosmos

Gyroscope Sensor for Measuring Angular Velocity Vector Projections-4

A redundant, free-form gyroscopic angular velocity vector meter designed for spacecraft orientation and stabilization control systems, featuring four independent measurement channe

Purpose	Measurement of angular increments (rate integral) on sensitive axes of four measurement ch
Year of release	2019
Guaranteed service life (years)	17
Flight qualification of the product	No
Brief history of flight qualification	The instrument is being developed for future spacecrafts.

price on request

Glavkosmos

High Precision GNSS Module

RTK/GNSS high-precision navigation module (GPS/GLONASS/Galileo, <0.01 m RTK, <0.2 m standalone, 9–36 V, 120 g, -40 to +85 °C). For automotive/transport applications.

Purpose	High-precision navigation for automotive technology with RTK and LSN signal support
Year of release	2017
Guaranteed service life, years	3
Estimated production/delivery time	8 months
Flight qualification	No

price on request

Glavkosmos

Inertial Measurement Unit

An Inertial Measurement Unit (IMU) designed for future manned spacecraft, providing precise measurement of velocity and angle increments using fiber-optic gyroscopes and vibrating

Purpose	Measurement of velocity and angle increments on three sensitive axes of fiber-optic gyrosc
Year of release	2015
Guaranteed service life	15 years
Flight qualification of the product	No
Brief history of flight qualification	The instrument is being developed for future manned spacecraft.

price on request

Glavkosmos

Kinetic Moment Reset System

A magnetic momentum-management system that calms a low-orbit spacecraft and dumps accumulated kinetic moment from the spacecraft body and flywheel engines using geomagnetic-field c

Year of release	2005
Guaranteed service life (years)	10
Estimated production / delivery time (months)	14
Flight qualification of the product	Yes
Flight heritage	As part of the Resurs-DK spacecraft

price on request

Glavkosmos

Kinetic Moment Reset System 1207

The Kinetic Moment Reset System 1207 is designed to calm low-orbit spacecraft and dissipate accumulated kinetic moment from the spacecraft body and flywheel engines. It consists of

Purpose	Calming the low-orbit spacecraft and dumping the accumulated kinetic moment from the space
Year of release	2014
Guaranteed service life	10 years
Estimated production / delivery time	14 months
Flight qualification of the product	Da

price on request

Glavkosmos

Nanosatellite Attitude Control

A nanosatellite attitude control unit designed to manage external magnetic coils integrated into solar panels, offering independent PWM signal generation for two axes.

Purpose	The unit is designed for controlling the external magnetic coils integrated in solar panel
Year of release	2016
Guaranteed service life (years)	1 year
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Navigation and Communication Module

ERA-GLONASS/GNSS vehicle telematics module (48 ch, GPS+GLONASS, GSM/UMTS, accelerometer, RS-485/232, 9–36 V, 120 g, -40 to +85 °C, <8 W).

Purpose	GNSS navigation, ERA-GLONASS emergency response, telemetry, and telematics for vehicles
Year of release	2019
Guaranteed service life, years	3
Estimated production/delivery time	6 months
Dimensions, mm	120×90×40

price on request

Glavkosmos

On-board GNSS Receiver with Interface Outputs

Multi-constellation GNSS board module (44 ch, GPS/GLONASS/Galileo/SBAS L1, 2.5 m 2Drms, 2×RS-232/LVCMOS, 71×51×12 mm, 10 g, 0.07 W). 4 hardware versions.

Purpose	Navigation and communications equipment
Year of release	2017
Guaranteed service life, years	3
Estimated production/delivery time	7 months
Dimensions, mm	71×51×12

price on request

Glavkosmos

Reaction Wheels Block

The Reaction Wheels Block is an executive part of a CubeSat three-axis orientation and stabilization system, containing four reaction wheels for precise attitude control.

Purpose	Executive part of CubeSat three-axis orientation and stabilization system.
Year of release	2018
Guaranteed service life (years)	1
Estimated production / delivery time (months)	5
Flight qualification of the product	No

price on request

Glavkosmos

Satellite Laser Ranging and Velocity Measurement System of Spacecraft

A laser ranging and velocity measurement system designed for spacecraft, enabling automatic docking by precisely measuring mutual arrangement parameters.

Purpose	Measuring of mutual spacecraft arrangement parameters for automatical docking.
Year of release	2020
Guaranteed service life (years)	It will be determined according to development result.
Estimated production / delivery time (months)	According to specified hardware components based on development result.
Flight qualification of the product	No

price on request

Glavkosmos

Small-sized navigation equipment GM

A compact GLONASS/GPS navigation receiver for determining current coordinates, ground speed and course of travel.

Operating temperature range	from -30 to +55
weight	0,32 kg
Power consumption	1 Wt
First determination time	90 sec
Frequency range of received channels	1,6 GHz

price on request

Glavkosmos

Small-sized Unit for Measuring Angular Velocity 1

The small-size block for measuring the angular velocity is designed to measure the integrals of the absolute angular velocity vector projections of the spacecraft when operating in

Measured angular velocity range	±8◦/s (Rough) ±4◦/s (Precise)
Output information impulse value	0,36±0,06 arc second (Rough) 0,18±0,024 arc second (Precise)
Certified zero signal value independent of overload	±610 arc second/s (Rough) ±60 arc second/s (Precise)
Random deviation of the zero signal at startup from the certified value	±16 arc second/s (Rough) ±3 arc second/s (Precise)
Noise component of the output signal in Precise mode	±2 arc second

price on request

Glavkosmos

Small-sized Unit for Measuring Angular Velocity 2

An upgraded version for KIND34-040. The small-size device for measuring the angular velocity is designed to measure the integrals of the absolute angular velocity vector projection

Measured angular velocity range	±4/s (Rough) ±2◦/s (Precise)
Output information impulse value	0,06..0,1 arc second (Rough) 0,03..0,05 arc second (Precise)
Certified zero signal value independent of overload	±610 arc second/s (Rough) ±60 arc second/s (Precise)
Random deviation of the zero signal at startup from the certified value	±16 arc second/s (Rough) ±3 arc second/s (Precise)
Noise component of the output signal in Precise mode	±0,15 arc second

price on request

Glavkosmos

Spacecraft orientation and stabilization system

A high-precision orientation and stabilization system for medium-orbit spacecraft, designed to manage spacecraft attitude, perform programmable turns, and ensure energy levels.

Year of release	2019
Estimated production / delivery time (months)	24
Flight qualification of the product	Yes
Brief history of flight qualification	"Condor-E" spacecraft
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Star Tracker GEO

The Star Tracker GEO is an autonomous star tracker designed for star-based satellite attitude determination, specifically for geostationary Earth orbit (GEO) applications.

Purpose	Star based satellite attitude determination.
Year of release	2019
Guaranteed service life (years)	5
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Star Tracker LEO

The Star Tracker LEO is an autonomous star tracker designed for satellite attitude determination in Low Earth Orbit (LEO) up to 1200 km, offering a guaranteed service life of 5 yea

Purpose	Star based satellite attitude determination
Year of release	2019
Guaranteed service life (years)	5
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Sun Sensor

The Sun Sensor is a two orthogonal axes digital sun sensor designed for nano-satellites, providing directional cosines of the sun's direction without requiring calibration.

Purpose	Designed for use in nano-satellites missions. CAN interface provides single cable connecti
Year of release	2017
Guaranteed service life (years)	1
Estimated production / delivery time (months)	3
Flight qualification of the product	Yes

price on request

Glavkosmos

VLSI kit for low-power GLONASS / GPS navigation receiver

Two-chip low-power VLSI kit (VLSI 1 + VLSI 2) for multi-channel combined GLONASS/GPS navigation receivers.

Dimensions	6×6×1 mm
Mass	1 g
Supply voltage	1.20 ± 0.12 V (core); 1.8 ± 0.18 V (I/O)
Operating temperature	-40°C to +85°C
Number of channels	36

price on request

GomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete 1U–12U satellite platforms. GomSpace has one of t

GomSpace

3-Axis Magnetorquer NanoTorque GST-600

The NanoTorque GST-600 is a compact three-axis magnetorquer designed for satellite attitude control, suitable for 6U CubeSats and other small satellites.

Dipole Moment (Z-axis)	typ. 0.5 Am²
Dipole Moment (X/Y-axis)	typ. 0.4 Am²
Temperature Sensor	Integrated
Size	91 x 97 x 17 mm
Mass	180 g

price on requestdatasheet

GomSpace

NanoSense FSS

The NanoSense FSS is an ultra-compact, low-power vector sun-sensor with an I2C interface, designed for precise two-axis solar angle measurements in CubeSat AOCS.

Form Factor	22 x 11 x 5 mm
Mass	2.2 grams
Interface	I2C

price on requestdatasheet

GomSpace

NanoSense M315

The NanoSense M315 is a flight-proven, compact, and low-noise magnetometer with an I2C interface, designed for nanosatellites requiring high AOCS performance.

Form factor	23 x 20 x 8 mm
Mass	8 grams
Flight heritage	flight-proven

price on requestdatasheet

GomSpace

NanoTorque GST-600

A compact three-axis magnetorquer combining a single air-torquer and two magnetorquer-rods for satellite attitude control, designed for 6U CubeSats and scalable to smaller and larg

Type	3-axis magnetorquer (1 air-torquer + 2 magnetorquer rods)
Target platform	Primarily 6U CubeSat (also usable in smaller/larger))
Torque	High torque, low residual dipole
Integration	Compatible with NanoTorque GSW-600 reaction wheels
Heritage	Flight-proven GomSpace product line

price on requestdatasheet

GomSpace

NanoTorque GSW-600

The NanoTorque GSW-600 is a compact, high-performance reaction wheel system consisting of four wheels in a pyramid setup, designed for 5 years of in-orbit operations for CubeSats a

Torque	2 mNm
Momentum	19 mNms
Maximum Speed	6000 rpm
Interface	SPI
Redundant Data Interface	I2C

price on requestdatasheet

GomSpace

NanoTorque GSW-600 Reaction Wheels

4-wheel pyramid reaction wheel assembly for CubeSats, flight-proven with a 5-year design lifetime and seamless integration with GomSpace ADCS ecosystem.

Configuration	4-wheel pyramid assembly
Design lifetime	5 years in-orbit
Integration	Compatible with NanoTorque GST-600 magnetorquer
Application	CubeSat 3-axis attitude control
Heritage	Flight-proven

price on requestdatasheet

Turkish space and aerospace technology company; satellite engineering services, space system components, and technical expertise for Turkey's growing commercial space sector.

Gumush

n-ART ST 1U Star Tracker

Gumush's n-ART ST 1U is a compact 0.1 kg star tracker for CubeSat and small satellite attitude determination, part of the n-ART family scaling from 1U to 3U form factors.

Mass	0.1 kg
Form factor	1U
Function	Autonomous star-field attitude determination
Product family	n-ART ST (1U, 2U, 3U variants)

price on request

Gumush

n-ART ST 2U Star Tracker

Gumush's n-ART ST 2U is a 0.2 kg star tracker for small satellite attitude determination, the mid-size member of the n-ART family covering 1U to 3U configurations.

Mass	0.2 kg
Form factor	2U
Function	Autonomous star-field attitude determination
Product family	n-ART ST (1U, 2U, 3U variants)

price on request

Gumush

n-ART ST 3U Star Tracker

Gumush's n-ART ST 3U is the largest star tracker in the n-ART family at 0.3 kg, offering the highest pointing accuracy for small satellite missions requiring precision attitude det

Mass	0.3 kg
Form factor	3U
Function	Autonomous star-field attitude determination
Product family	n-ART ST (1U, 2U, 3U variants)

price on request

Indian small satellite manufacturer offering flight-proven platforms, subsystems, and mission-as-a-service solutions.

HEX20

Star Tracker

Compact radiation-tolerant star tracker for micro/small satellites — ~16 arcsecond pointing accuracy, star detection to magnitude 6, 325g mass, compatible with any third-party ADCS

Field of view	10°x10°
Update rate	5 Hz
Dimensions	95x85x85 mm
Star detection	Up to magnitude 6.0
Pointing accuracy	~16 arcseconds

price on request

Swedish technology company providing precision measurement, geospatial, and positioning solutions including satellite navigation systems.

Italian developer of autonomous attitude determination systems (star trackers) for small satellites.

Hipparcos S.r.l.

ARGO 1.0 Star Tracker

Flight-proven multicamera autonomous attitude determination system (star tracker) for small satellites.

Interface	RS422, SpaceWire, CANBus (redundant)
Flight heritage	In-orbit demonstration on D-Orbit ION SCV2, launched Jan 2021, validated through Jul 2022
TRL	8 (flight-demonstrated)
Validated functions	Pattern recognition, tracking-mode accuracy, straylight robustness, Moon/Earth-in-FOV hand

price on requestdatasheet

Honeywell Aerospace is a major division of Honeywell International Inc. (NASDAQ: HON) — a Fortune 100 conglomerate headquartered in Charlotte, North Carolina — providing avionics, satellite navigation equipment, satellite communications sys

Honeywell Aerospace

HMC2003 3-Axis Magnetometer

A high-sensitivity, factory-calibrated analog 3-axis magnetometer from Honeywell used for precision magnetic field measurement in navigation and attitude reference applications.

Axes	3 (X, Y, Z)
Field Range	+/-2 gauss
Resolution	40 microgauss
Package	20-pin hybrid DIP
Sensor Elements	HMC1001, HMC1002 magnetoresistive sensors

price on requestdatasheet

Honeywell Aerospace

HMR2300 3-Axis Magnetometer

The HMR2300 is a three-axis smart digital magnetometer that measures the strength and direction of magnetic fields for attitude reference, compassing, and navigation applications.

Axes	3 (X, Y, Z)
Field Range	+/-2 gauss
Resolution	<0.1 milligauss
Output	16-bit digital
Interface	RS-232 (full-duplex) or RS-485 (half-duplex)

price on requestdatasheet

Honeywell Aerospace

HR04, HC7 & HC9 Reaction Wheel Assemblies

The HR04, HC7, and HC9 are a series of reaction wheel assemblies designed for spacecraft attitude control, offering flexibility in packaging, momentum, and torque options.

Gen 1 Qualification (HC7 and HC9)

Completed in June 2021

price on request

Honeywell Aerospace

Momentum Control Systems

Honeywell's Momentum Control Systems offer turnkey controls for arrays of up to six Control Moment Gyroscopes (CMGs), ensuring deterministic, singularity-free operation with guaran

Rotor Momentum	50 ft-lb-sec
Peak Torque	50 ft-lb
Gimbal Rate	1 rad/sec
Power Consumption	120 W
Slew Rate	up to 15 deg/min

price on request

Indra Space is the space division of Indra Group — a European prime contractor with 40+ years delivering end-to-end space solutions across Earth observation, satellite navigation, telecommunications, space surveillance, and exploration for

Indra Sistemas

READY ADCS

Indra's READY ADCS is a turnkey attitude determination and control system for small satellites and CubeSats, designed for high precision and agility in LEO orbits.

Designed for	Small satellites and CubeSats
Orbit compatibility	All LEO orbits
Configurations	READY-200, READY-100, READY-16U, READY-6U

price on request

Irish manufacturer of high-performance inertial sensors and systems for space, aerospace, and defence applications.

Innalabs

AI-Q-2020 Navigation Grade Quartz Accelerometer (±60g, 220 µg)

Navigation-grade quartz accelerometer, ±60g, <220 µg bias repeatability, with temperature compensation.

Input Range	±60 g
One-year Bias Repeatability	<220 µg
Temperature Sensitivity (Bias)	<30 µg/°C
Scale Factor Repeatability	<500 ppm
Axis Misalignment Repeatability	<100 µrad

price on request

Innalabs

AI-Q-2030 Navigation Grade Quartz Accelerometer (±60g, 160 µg)

Navigation-grade quartz accelerometer, ±60g, <160 µg bias repeatability, internal temperature model.

Input Range	±60 g
Bias	≤4 mg
One-year Bias Repeatability	≤160 µg
Temperature Sensitivity (Bias)	≤30 µg/°C
Scale Factor	1.2 to 1.46 mA/g

price on request

Innalabs

AI-Q-550 Control Grade Quartz Servo Accelerometer (±80g)

Miniature control-grade quartz accelerometer, ±80g, <1000 µg bias repeatability, 250g shock, 25.8g.

Input Range	±80 g
Bias	<4 mg
One-year Bias Repeatability	<1000 µg
Temperature Sensitivity (Bias)	<50 µg/°C
Scale Factor	0.65 to 0.85 mA/g

price on request

Innalabs

ARIETIS

ARIETIS is an ITAR-free, space-qualified, rad-hard 3-axis gyroscope designed for use as a primary gyro or coarse rate sensor in various Earth orbits and space missions. It provides

Measurement Range	[-3°/s; +3°/s] fine mode [-48°/s; +48°/s] coarse mode
Switch-on response time	≤ 6s
ARW	≤ 0.005°/√hr
In-run bias stability	≤ 0.1°/hr
Bias Stability over 24hr (steady temperature)	≤ 1.5°/hr (1σ)

price on request

Innalabs

ARIETIS-NS 3-Axis Rad-Tolerant Space Gyroscope System

Space-qualified 3-axis CVG for LEO/GEO/MEO, 30krad TID, ITAR-free, serial production, 16-year lifetime.

Measurement Range	[-12°/s; +12°/s]
Switch-on Response Time	≤6 seconds
Angular Random Walk (ARW)	≤0.005°/√hr
In-run Bias Stability	≤0.1°/hr
Bias Errors (3σ)	≤10°/hr

price on request

Innalabs

GI-CVG-A23XXD A-Series 3-Axis CVG Digital Gyroscope

3-axis Coriolis Vibratory Gyroscope with RS422 digital output, 0.3°/hr bias stability, 500K+ hr MTBF.

Input Rate	±160°/s
Bias In-Run (1σ)	0.3°/hr
Angle Random Walk (ARW)	0.01 °/√hr typical
Bandwidth (-3dB)	>300 Hz
Turn-on Time	1 sec

price on request

Innalabs

GI-CVG-N-Series 1 & 2-Axis Gyroscope (Tactical/Industrial Grade)

1 or 2-axis CVG with <10°/hr full-temp bias stability, <0.22°/hr in-run, 500K+ hr MTBF.

In-run Bias Stability (room temp, 1σ)	<0.22 deg/hr
Bias Stability – Tactical (full temp, 1σ)	<10 deg/hr
Bias Stability – Industrial (full temp, 1σ)	<50 deg/hr
Scale Factor Error (full temp, 1σ)	<3,500 ppm
Scale Factor Linearity	≤1500 ppm

price on request

Innalabs

GI-CVG-U-Series 1 & 2-Axis Gyroscope

1 or 2-axis tactical CVG, <10°/hr full-temp bias stability, <0.22°/hr in-run, RS-422 or analog output.

In-run Bias Stability (room temp, 1σ) – Tactical	<0.22 deg/hr
Bias Stability – Tactical (full temp, 1σ)	<10 deg/hr
Bias Stability – Industrial (full temp, 1σ)	<50 deg/hr
Scale Factor Error (full temp, 1σ)	<3,500 ppm
Angular Random Walk	0.01 deg/√hr typical

price on request

ISISPACE provides launch services, manufactures CubeSat deployers and other launch equipment, and acts as a satellite systems integrator for small satellites.

Innovative Space Logistics

ISISPACE GNSS Patch Antenna

The ISISPACE GNSS Patch Antenna is a compact, low-mass, and flight-proven antenna designed for GPS-L1 and GALILEO-E1, offering pinpoint positioning for CubeSats.

price on requestdatasheet

Bengaluru-based space startup offering end-to-end CubeSat design, manufacturing, subsystem development, and ground station services for nanosatellite missions.

ISpaceI Satellite and Research

ISpaceI ADCS — Attitude Determination and Control System

Compact ADCS for 1U–3U CubeSats providing three-axis attitude determination and control.

Compatible form factors	1U, 2U, 3U CubeSat
Control type	Three-axis active attitude control
Integration	Compatible with ISpaceI OBC and EPS subsystems
Mounting	Internal CubeSat frame
Target orbit	Low Earth Orbit (LEO)

price on request

American GNSS technology company manufacturing high-precision positioning receivers for surveying, geodesy, and machine control applications.

JAVAD GNSS

JAVAD GNSS

JAVAD GNSS is a designer and manufacturer of multi-constellation, multi-frequency GNSS receivers for demanding industrial applications, including a board specifically designed for

Channels	874
Cellular	Internal 4G/LTE/3G
Radio	UHF 1W transceiver
Wi-Fi	5GHz/2.4GHz (802.11 a/b/g/n/d/e/i)
Bluetooth	Dual-mode + BLE

price on requestdatasheet

Jena-Optronik designs and manufactures sensors, space optics, and electronics for satellites and spacecraft, supporting communication, navigation, and Earth observation.

Jena-Optronik

ASTRO APS Autonomous Star Sensor

Heritage autonomous star sensor for LEO-GEO-deep space: <1/18yr lifetime, >470 units contracted including NASA Orion/Artemis.

Field of View	20 deg circular
Optics	Refractive, 43mm focal length, f/1.2, rad-hard glass
Detector	1024x1024 px; HAS2 or STAR1000 APS CMOS
Attitude Random Error XY (1-sigma)	<1 arcsec
Attitude Random Error Z (1-sigma)	<8 arcsec

price on request

Jena-Optronik

ASTRO APS3 Autonomous Star Sensor

Next-gen Jena-Optronik star tracker: 1.8kg, <6W, 20deg FOV, <0.8/<7 arcsec XY/Z accuracy, <1s lost-in-space acquisition, 7.0 mi sensitivity, 8-16 Hz, SpaceWire/1553/RS4

Field of View	20 deg full-cone (circular)
Optics	Refractive, 29mm focal length, f/1.0
Image Sensor	FaintStar2 SoC, 1024x1024 px
Update Rate	8, 10, or 16 Hz
Accuracy (XY/Z, 1-sigma total)	<=0.8 / 7.0 arcsec (at <0.1 deg/s)

price on request