Space Hardware Marketplace

MACM Attitude Control Magnetometer

Compact tri-axial fluxgate magnetometer for LEO satellite attitude determination, 249 g, 28 V RS485 interface.

SBCFA1000 Single-Board Computer

• TypeRadiation-tolerant single-board computer (OBC)
• ApplicationCommand and data handling, payload management
• HeritageNASA ISS research activities (400+ experiments)

Flight-proven radiation-tolerant single-board computer for satellite command, data handling, and payload management.

PDUFA1000 Power Conditioning and Distribution Unit

• TypePower Conditioning and Distribution Unit (PCDU)
• HeritageISS, Space Shuttle, NASA Artemis (Lunar Gateway)
• Quality StandardAS 9100-registered

Spaceflight-heritage power conditioning and distribution unit (PCDU) for satellite and spacecraft applications.

Copper Flexible Thermal Straps

• MaterialCopper
• TypeFlexible Thermal Strap (FTS)
• Temperature RangeCryogenic to room temperature

Robust copper flexible thermal straps for space thermal management, qualified for cryogenic and room-temperature applications.

PSG Thermal Links (Pyrolytic Graphite Flexible Thermal Straps)

• MaterialPyrolytic Graphite Sheet (PGS)
• TypeFlexible Thermal Strap (FTS)
• ApplicationsFocal plane assemblies, cryo-cooler interfaces, deployable radiators

High-performance pyrolytic graphite flexible thermal straps for space applications requiring high thermal conductance with minimal mass.

Akash Ka-S CubeSat Radio

• Frequency BandsKa-band (downlink) + S-band (uplink)
• Radio TypeSoftware-Defined Radio (SDR)
• Cooling TechnologyDiamond Cooling (GaN-on-Diamond)

Ka/S-band dual-frequency CubeSat software-defined radio enabling high-rate downlink and S-band command uplink.

Akash Space Power Amplifier

• Cooling TechnologyDiamond Cooling (GaN-on-Diamond)
• Peak Power Improvement2-3x vs conventional
• Energy Efficiency Improvement~50% vs conventional

GaN-on-Diamond space power amplifier with ~50% greater energy efficiency and 2-3x higher peak power for satellite RF payloads.

Akash CubeSat Radio

• Dimensions100 x 100 x 30 mm
• Max Downlink Data Rate700 Mbps (extendable to 1.4 Gbps)
• Max Power Consumption< 28 W

GaN-on-Diamond CubeSat satellite radio with up to 700 Mbps downlink in a 10 x 10 x 3 cm…

ARIETIS 3-Axis Rad-Hard Gyroscope System

• Axes3
• Measurement Range (fine)+/-3 deg/s
• Measurement Range (coarse)+/-48 deg/s

ITAR-free 3-axis radiation-hardened inertial reference unit for GEO/LEO/MEO satellites, bias stability <= 0.1 deg/hr.

AQUILA Space-Qualified Rad-Hard Accelerometer

• TechnologyQuartz Flexure Servo Accelerometer
• RadiationRad-Hard
• Development ContractESA (2019)

ESA-developed radiation-hardened quartz servo accelerometer for space inertial navigation and AOCS.

Earth Horizon Sensor

The Pyxis Space Earth Horizon Sensor provides nadir-vector measurement for CubeSat attitude control using both visible (VIS) and…

SmartMEO

• OrbitMedium Earth Orbit (MEO), ~23,616 km, 56° inclination
• Launch Mass~733 kg
• Propulsion8x 1 N hydrazine thrusters

Medium-Earth-orbit navigation satellite platform proven on 34 Galileo FOC satellites at ~23,616 km altitude.

Heinrich Hertz (H2Sat) Platform

• OrbitGeostationary Earth Orbit (GEO)
• Launch Mass~3,408 kg
• Platform BusSmallGEO (LUXOR)

Advanced GEO technology-demonstration satellite based on SmallGEO bus, hosting flexible in-orbit verification payloads for DLR.

Reaction Wheel

The Pyxis Space Reaction Wheel is a miniaturized momentum exchange device for precise attitude control of CubeSat and…

SmallGEO

• OrbitGeostationary Earth Orbit (GEO)
• Launch Mass~3,200–3,500 kg
• Dry Mass~1,700 kg

European small geostationary satellite platform for commercial telecommunications missions up to 3,500 kg launch mass.

SmartLEO

• OrbitLow Earth Orbit (LEO), including Sun-Synchronous Orbit (SSO)
• Typical Mass Range~770–940 kg
• Typical Orbit Altitude470–650 km

Flexible LEO satellite platform for Earth observation and reconnaissance missions, proven on SAR-Lupe and EnMAP.

VES16 11S16P Battery

• ChemistryLi-ion
• Cell Configuration11S16P
• Capacity288 Ah

High-capacity 11,264 Wh / 288 Ah space lithium-ion battery for large satellite platforms.

MP & VL Batteries for Launchers

• ChemistryLi-ion
• Cell FormatsPrismatic (MP), Cylindrical (VL)
• VL Power VariantsPower (P), Very High Power (U)

Launcher-qualified prismatic MP and cylindrical VL rechargeable lithium-ion batteries for space launch vehicles.