Space Hardware Marketplace

STARS-II (Space Tethered Autonomous Robotic Satellite II)

• ConfigurationMother (2U) + Daughter (1U) CubeSat pair
• TetherKevlar, 300 metres
• LaunchFebruary 2014 (HTV-3 to ISS)

Kyoto University / Shizuoka University tethered satellite pair — Mother and Daughter CubeSats demonstrating space tether technology deployed…

SwissCube

• Form factor1U CubeSat
• Mass820 g
• Dimensions10 × 10 × 10 cm

Switzerland's first satellite — 1U CubeSat measuring atmospheric airglow, launched September 2009, operational for over a decade.

MOVE-II

• Form factor1U CubeSat
• Mass~850 g
• Dimensions10 × 10 × 10 cm

TUM's second student-built CubeSat — 1U nanosatellite launched December 2018, demonstrating atmospheric drag measurement and lithium battery degradation…

Milani

• Form factor6U CubeSat
• Mass~8 kg
• Launch dateOctober 7, 2024

ESA Hera mission CubeSat built by PoliMi — 6U nanosatellite deployed at the Didymos binary asteroid system to…

FDSS

• InterfaceDigital
• Full Field of View140° × 140°
• AccuracyBetter than 0.1°

Fine Digital Sun Sensor immune to Earth albedo, captures Sun images in <1 ms, 140×140° full field of…

MicroST

High-precision star tracker for microsatellites with <6 arcsec XY accuracy, multi-camera support and LEO/MEO/GEO qualification.

nanoST

Compact plug-and-play star tracker for nanosatellites with <40 arcsec XY accuracy and 15° field of view.

HSNS

• InterfaceUART or I2C, microD 15 pins
• Field of View±64°
• Supply voltage5 V, 150 mW peak

Quad-thermopile horizon sensor for nadir vector determination and attitude control on nanosatellites and microsatellites.

ACSS RH

• InterfaceAnalog
• Flight modeYes
• Engineering modeYes

Radiation-hardened Advanced Coarse Sun Sensor qualified to 200 krad for MEO and GEO missions.

ACSS

• InterfaceAnalog
• Flight modeYes
• Engineering modeYes

Advanced Coarse Sun Sensor for sun-tracking and attitude determination, flight-proven since 2019 with hundreds of units delivered.

SSOC D60

• InterfaceDigital
• Field of View±45° or ±60°
• Supply voltage5 V, 75 mA

MEMS-based digital fine sun sensor with ±45°/±60° FOV and digital output of sun angles without external calculations.

SSOC A60

• InterfaceAnalog
• Flight modeYes
• Engineering modeYes

MEMS-based analog fine sun sensor with ±60° FOV, calibrated with look-up table, for high-accuracy attitude determination.

nanoSSOC D60

• InterfaceDigital (UART, I2C, SPI)
• Field of View±60°
• Supply voltage3.3 V or 5 V

Two-axis MEMS-based digital sun sensor for CubeSats with UART/I2C/SPI output and ±60° field of view.

nanoSSOC A60

• InterfaceAnalog
• Flight modeYes
• Engineering modeYes

Two-axis MEMS-based analog sun sensor for CubeSats and nanosatellites with ±60° field of view.

CANSAT Transmitter Module

• Frequency Bands2m, 70cm, 916 MHz
• Supply voltage5 to 12 volts
• Data InterfaceUART at 38.4 Kbits/sec

Low-cost, low-power AX.25/APRS RF transmitter module for CanSat and small satellite projects.

StenSat Radio Beacon

Small AX.25 FM telemetry beacon for CubeSats and small satellites.

Aurora Earth Observation Studio

• DeploymentCloud-native, browser-based
• Preset spectral indices20+
• Pricing (Standard)Free

Cloud-native no-code platform for tasking, visualising, and analysing Pixxel hyperspectral imagery — with 20+ preset spectral indices, AI/ML…

Solstar LWIFI-X — Lunar WiFi Access Point

• TypeRadiation-hardened WiFi access point
• RatingSpace-rated and human-rated
• ProtocolWiFi (802.11)

Radiation-hardened, space-rated WiFi access point for lunar rovers, surface habitats, space stations, and crewed vehicles — developed under…