Space Hardware Marketplace

SpooQies

• Payload typesEntanglement-based QKD and Prepare-and-Measure QKD
• Flight heritageBased on SpeQtral-1 satellite design
• DeliveryOrbital delivery included

Turnkey QKD satellite or constellation based on the flight-proven SpeQtral-1 design, supporting entanglement-based and prepare-and-measure QKD payloads for…

InGaAs PIN Photodetector Die

• MaterialInGaAs P-I-N on InP substrate
• Active area sizes25 µm to 1 mm diameter
• Wafer sizes2", 3", and 4" InP substrates

Telcordia-qualified InGaAs P-I-N photodetector device dies for telecom, laser power monitoring, and test systems, available in 25 µm…

Space Solar Arrays

• IntegrationFully integrated and tested — delivered assembly-ready
• Cell technologyXTE and XTJ family multijunction cells
• Test capabilityLAPSS II large area pulsed solar simulator (up to 12 ft diameter panels)

Fully integrated and tested space solar arrays delivered to satellite primes for direct spacecraft integration, manufactured with Spectrolab's…

2V GaAs Laser Power Converter

Dual-junction GaAs photovoltaic converter optimized for 810 nm laser light, achieving 50–55% conversion efficiency for power-over-fiber and laser…

XTJ Prime Solar Cell

• BOL efficiency (average)30.7%
• EOL efficiency at 1e15 fluence26.7%
• Cell technologyHeritage upright lattice matched XTJ triple-junction

Spectrolab's proven heritage triple-junction solar cell with 30.7% average BOL efficiency, dual-qualified under AIAA-S111 and AIAA-S112, available in…

Space Solar Panels

• IntegrationMultijunction solar circuits bonded to customer-furnished substrate
• OptimizationEngineered for maximum EOL performance per mission profile
• Cell technologyXTE or XTJ family multijunction cells

Fully assembled space solar panels built to customer specifications, integrating Spectrolab's multijunction solar cells for maximum EOL performance…

XTE+ LEO Solar Cell

• BOL efficiency33%
• EOL efficiency at 1e14 fluence30.6%
• Cell technologyGaInP/GaAs/Ge lattice matched triple-junction (3J)

Spectrolab's 33% BOL efficiency triple-junction solar cell optimized for LEO missions with lower radiation fluence (<1e14), achieving 30.6%…

XTE-SF Solar Cell

• BOL efficiency32%
• EOL efficiency at 1e15 fluence27.9%
• Cell technologyGaInP/GaAs/Ge lattice matched triple-junction (3J)

Spectrolab's XTE Standard Fluence 32% BOL triple-junction solar cell for GEO and LEO missions up to 1e15 fluence,…

XTE-HF Solar Cell

• BOL efficiency32%
• EOL efficiency at 1e16 fluence23.6%
• Cell technologyGaInP/GaAs/Ge lattice matched triple-junction (3J)

Spectrolab's XTE High Fluence 32% BOL triple-junction solar cell for MEO and very high radiation environments exceeding 1e15…

XTE-LILT Solar Cell

• BOL efficiency (1 AU)32%
• Efficiency at jupiter lilt conditions37%
• Cell technologyGaInP/GaAs/Ge lattice matched triple-junction (3J)

Spectrolab's triple-junction solar cell optimized for Low Intensity Low Temperature conditions, achieving 37% efficiency at Jupiter for deep…

XTE+ GEO Solar Cell

• BOL efficiency33%
• EOL efficiency at 1e15 fluence28.5%
• Cell technologyGaInP/GaAs/Ge lattice matched triple-junction (3J)

Spectrolab's latest 33% BOL efficiency triple-junction solar cell optimized for GEO and high-radiation missions (>1e14 fluence), fully qualified…

CANDELABRA

• System typeArtificial sun simulator / precision lighting array
• Simulated environmentLunar south pole lighting conditions
• Coverage area30 × 20 m

Precision artificial sun simulator for the ESA-DLR LUNA Analog Facility in Cologne, replicating the grazing-angle, high-contrast lighting conditions…

LISE Airlock

• ArchitectureHybrid rigid + deployable (inflatable) structure
• ApplicationEVA crew ingress/egress at lunar surface
• Host habitatLISE (Lunar Integrated Shelter for Exploration) atop a robotic lander

Deployable lunar surface airlock with hybrid rigid-inflatable architecture for the LISE habitat, enabling safe EVA crew ingress/egress with…

EUROSUIT

• Suit typeIntra-Vehicular Activity (IVA)
• ApplicationLaunch, landing, and emergency phases inside crewed spacecraft
• Don/doff time<2 minutes (autonomous, unassisted)

Europe's first IVA space suit prototype designed for launch and landing protection aboard crewed spacecraft, featuring autonomous donning/doffing…

EUROHAB

Inflatable, deployable lunar surface habitat delivered as payload by a robotic lander, serving as an outpost, emergency refuge,…

LaserCube Laser Communication Terminal

2U laser communication terminal for CubeSats and small satellites delivering >10× higher throughput than RF solutions. Flight-proven on…

EWC27 X-Band Transmitter

High-data-rate X-Band transmitter for CubeSats and nanosatellites supporting up to 140 Mbps. ITAR-free, TRL 9, 120+ flight models.

EWC31-NG S/S-Band Transponder

Next-generation S-Band TT&C transponder for CubeSats and nanosatellites with radiation hardening and ITAR-free design.