Space Hardware Marketplace

Space INSPIRE

• OrbitGeostationary orbit
• PropulsionAll-electric
• ReconfigurabilityFull in-orbit digital reconfiguration of coverage, capacity and beams

Fully digital, in-orbit reconfigurable geostationary telecommunications satellite platform.

Spacebus NEO

All-electric geostationary telecommunications satellite platform with modular design and high payload power.

Terra Space Lab Environmental Monitoring Services

Terra Space Lab provides global space-based multispectral environmental monitoring services, focusing on wildfire detection, forest monitoring, and climate…

Rigel 500

The Rigel 500 is a bipropellant thruster offered by Tesseract Space, designed for SmallSat propulsion subsystems.

Lyra 22

The Lyra 22 is a bipropellant thruster designed for SmallSat propulsion subsystems, offered by Tesseract Space.

Lyra 1

Lyra 1 is a bipropellant thruster designed for SmallSat propulsion subsystems, offered by Tesseract Space.

PocketQube Satellite Structure

• Form factors1P, 2P, 3P PocketQube
• Compatible deployerMR-FOD
• Launch platformItalian UniSat micro-satellite

Standard PocketQube satellite structures in 1P, 2P, and 3P sizes for launch via the MR-FOD deployer.

MR-FOD Deployer

• TypePocketQube deployer
• Manufacturing method3D printed
• Launch partner platformItalian GAUSS Team UniSat micro-satellite

3D-printed PocketQube deployer, the standard launcher for PocketQubes on the Italian GAUSS Team UniSat micro-satellite.

Teton CubeSat Deployer

• TypeCubeSat deployer
• Design featureNo corner-capturing / square-section requirement, allowing flexible solar panel mounting

Next-generation CubeSat deployer offering greater flexibility for solar panel placement.

Tu-POD Deployer

• TypePicoSat / PocketQube sub-deployer
• Host interfaceFits inside a standard P-POD

First-generation Teton deployer fitting inside a standard P-POD to launch PicoSats and PocketQubes.

1N HTP Monopropellant Thruster

1 N monopropellant thruster running on 98% high-test peroxide, developed at Łukasiewicz - ILOT and commercially produced by…

420N HTP Bipropellant Kick-Stage Engine

420 N-class bipropellant rocket engine using 98% hydrogen peroxide as oxidizer, developed under ESA's GRACE 1/2 programs and…

Highly concentrated, pure hydrogen peroxide

• Concentration range80% up to 99.99%
• Dedicated for in-space propulsion systems98% HTP

Thaliana Space offers highly concentrated hydrogen peroxide (HTP) ranging from 80% to 99.99%, with 98% HTP specifically designed…

High Test Peroxide (HTP)

• Concentration range80% to 99.99%
• Recommended grade for in-space propulsion98% HTP

Highly concentrated, pure hydrogen peroxide (HTP) propellant offered in concentrations from 80% up to 99.99%, with a 98%…

Green Propulsion System (4x1N HTP Monopropellant Module)

Blowdown monopropellant propulsion system using 98% HTP with four 1 N thrusters for LEO small-satellite orbital maneuvers, attitude…

LPT 9310 HP COTS+

The LPT 9310 HP COTS+ from Thales Group is a Pulse-Tube Cryocooler designed for space applications, offering a…

LPT 9510 COTS+

The LPT 9510 COTS+ is a Split Pulse-Tube Cryocooler designed for space and scientific applications, offering 1.4 W…

LPT6510 Pulse-tube Cryocooler

Designed-for-manufacturability pulse-tube cryocooler for 60 K and above, based on the flight-proven MPTC compressor.