| Featured Space and Satellite Products |
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| Closed Boundary Quad-Ridge Horn Antenna from 2 to 18 GHz | |
Satellite Antenna
from Microwave Vision Group
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| The QR2000-SPQ from Microwave Vision Group is a quad-ridge horn satellite antenna designed to support wideband space connectivity applications across multiple orbital regimes. Operating over a broad frequency range of 2 to 18 GHz, this closed-boundary antenna supports dual linear polarization and delivers gain performance from 7-21 dBi, enabling reliable RF operation for satellite communication and measurement use cases. This space-qualified antenna offers stable electrical performance across its operating band, maintaining a VSWR of less than 1.9 and a return loss better than -10 dB. |
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| Thermal Conditioning Unit for Space Simulation | |
Thermal Vacuum Chamber
from Telstar
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| The Thermal Conditioning Unit from Telstar is an advanced thermal control system designed to precisely regulate temperature conditions within space simulation environments. It plays a critical role in thermal vacuum chambers by accurately replicating the extreme thermal conditions encountered during space missions, enabling reliable testing and validation of spacecraft components and subsystems. This thermal conditioning system utilizes high-performance fluid recirculation technologies, including silicone oil and dense gaseous nitrogen (GN2), to ensure efficient and uniform thermal distribution. |
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| 5.5–19.4 nH Space-Qualified Air Core Inductors | |
Space Qualified Inductor
from Coilcraft
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| The AE360RAS series from Coilcraft is a range of space-qualified air core inductors designed for high-frequency RF and microwave applications. Covering an inductance range of 5.5–19.4 nH with a tolerance of ±5.2%, these inductors provide stable and precise inductive performance for spaceborne electronic systems. These inductors feature low DC resistance ranging from 3.4 to 10 mΩ and offer an SRF between 3.2–4 GHz, ensuring reliable operation across high-frequency circuits. With a maximum current rating of 2.9 A and a high Q factor of up to 75, they support efficient energy transfer and minimal losses in RF applications. |
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| Assembly JIG for CubeSats | |
Assembly JIG for Satellite
from NPC SPACEMIND
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| The TP12 from NPC SPACEMIND is an Assembly JIG designed for integration and testing of CubeSat platforms, supporting a 12U form factor with a payload mass capacity of up to 24 kg. Engineered for precision assembly and subsystem validation, it consists of a test pod, regulation plate and assembly screws, enabling efficient handling and alignment of satellite components during development and pre-launch preparation. This modular assembly platform incorporates an optional form factor reducer that enhances accessibility and simplifies integration across varying CubeSat configurations. |
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| MicroSat-Class Hinge System | |
Satellite Deployer
from EXA (Ecuadorian Space Agency)
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| The Hinges Micro L from EXA is a MicroSat-class hinge system designed for reliable deployment operations in satellite structures, including solar panels, antennas and other articulated subsystems. Engineered for precision and durability, it ensures controlled and repeatable deployment in space environments. It features hard-stop deployment angles defined during manufacturing, ensuring accurate positioning with a maximum angular deviation of ±1°. Compact and robust, the hinge measures 100 mm in length with a nominal thickness of 5 mm and weighs approximately 150 g, making it ideal for MicroSat platforms. |
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| 150 V Schottky Center-Tap Rectifier | |
Space Qualified Diode
from Solid State Devices
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| The SSR7015CTM from Solid State Devices is a space-qualified Schottky center-tap rectifier designed for high-efficiency power conversion in aerospace and high-reliability electronic systems. It supports an average rectified forward current of 35 A and a repetitive peak reverse voltage of 150 V, enabling robust performance in demanding power applications. The SSR7015CTM is assembled in a hermetically sealed TO-254 package and is also available in a surface-mount configuration, ensuring mechanical durability and reliability in harsh operating environments. The design supports stable electrical performances. |
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| Multi Band VSAT Terminal | |
Satellite Terminal
from Hughes Network Systems
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| The HT2500 from Hughes Network Systems is a Satellite Modem designed for enterprise and data center deployments, supporting operation across C, Ku and Ka-band satellite communication networks. It features DVB-S2X with Adaptive Coding and Modulation (ACM), enabling high spectral efficiency with symbol rates up to 235 Msps and modulation schemes ranging from QPSK to 32APSK, ensuring reliable and high-throughput satellite connectivity. It integrates advanced channel capabilities, including an MF-TDMA return channel supporting OQPSK and 8PSK modulation with LDPC forward error correction. |
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| 8-Channel Dual-Redundant PCDU | |
Power Conditioning and Distribution Unit (PCDU)
from Spaceteq
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| The EOS1 Power Distribution Unit from Spaceteq is a dual-redundant 8-channel power control and distribution unit designed for spacecraft operating in low Earth orbit. Engineered for high reliability, this unit ensures efficient power management and protection for onboard subsystems in mission-critical space environments. This power distribution features eight independently controlled tripping power switch channels, providing load management with integrated latch-up protection through trip signal feedback. The unit is designed with an interlocked switch bank control and consumes less than 3 W of power. |
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| High Performance Launch Lock Actuator | |
Space Actuator
from Nimesis
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| The TRHT02 from Nimesis is a high-performance miniaturized launch lock actuator designed for reliable deployment and release mechanisms in space systems. Based on Shape Memory Alloy (SMA) technology, it provides precise and controlled actuation, supporting a maximum axial preload of up to 1265 N and a fracture load of 1800 N, ensuring secure restraint and dependable release under demanding launch conditions. This space-grade actuator operates through thermal triggering, with an activation temperature of approximately 150°C and a configurable actuation time ranging from 30 to 300 seconds. |
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| High performance GNC platform for ADCS | |
ADCS System
from SkyLabs d.o.o.
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| The NANOadcs from SkyLabs d.o.o. is a high-performance guidance, navigation, and control platform designed as a complete Attitude Determination and Control System (ADCS) for small satellites. Featuring a compact and highly integrated architecture, the system incorporates a fault-tolerant 32-bit RISC-V onboard computer that executes advanced GNC algorithms, enabling precise attitude determination and high-accuracy pointing for modern satellite missions. This integrated ADCS solution combines a multi-constellation GNSS receiver with onboard sensors such as a magnetometer and gyroscope. |
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