Space Hardware Marketplace

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…

HTP Catalyst Systems

• Compatible HTP grades80-99%
• Decomposition timeWithin milliseconds
• Decomposition methodCatalytic (dedicated catalyst bed) or thermal

Catalyst systems for all HTP grades (80-99%) providing near-instantaneous (millisecond-scale) decomposition of hydrogen peroxide for monopropellant and bipropellant…

High-Test Peroxide (HTP) Propellant

• Concentration range80% up to 99.99%
• In-space propulsion grade98% HTP
• Supply modelDirect supply, or lease of dedicated on-site HTP production units for high-volume/long-duration customers

Highly concentrated hydrogen peroxide propellant, 80% up to 99.99%, with a 98% HTP grade dedicated to in-space propulsion…

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+ Pulse-Tube Cryocooler

5.7 W split pulse-tube cryocooler based on flexure-bearing technology, flown on NASA's ECOSTRESS instrument on the ISS.

LPT 9510 COTS+ Pulse-Tube Cryocooler

Compact split pulse-tube cryocooler delivering 1.4 W of cooling power at 80 K for IR detector cooling.

LPT6510 Pulse-tube Cryocooler

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

Cold Plates

• MaterialsAl and Al composites (0 to T6 temper, most common); Cu and Cu composites incl. Copper-Molybdenum; stainless steel
• Working fluidsDeionized water (with corrosion inhibitors and internal channel chem film); EGW; PGW; PAO
• Heat flux capabilityUp to 50 W/cm² (higher when integrated with an oscillating heat pipe)

Single- and two-phase pumped fluid cold plates for high-power electronics, from simple welded and inlaid-tube designs to complex…

OHP Radiators

Oscillating heat pipe (OHP) embedded spacecraft radiators and structural panels for on-orbit waste-heat rejection, delivering up to 9x…

OHP Chassis

Oscillating heat pipe (OHP) embedded electronics chassis and enclosures that structurally house circuit cards, RF modules, and Li-ion…

OHP Heat Frames

Oscillating heat pipe (OHP) embedded structural heat frames for VPX/VITA circuit cards and RF/power electronics, offering up to…

Cyclops

• Positioning accuracy< 50 m
• Max demonstrated altitude1.1 km
• Max demonstrated range104 km

Cyclops is a software-only visual positioning system (VPS) that gives fixed-wing UAVs reliable position estimates when GPS is…

ThinSat 300

Ku-band VICTS phased array antenna for comms-on-the-move, mounting on standard vehicle roof racks for satellite broadband at highway…