6213 satellite platforms, components and ground equipment from manufacturers worldwide.
This page offers various CubeSat Kit™ components specifically designed for the ISIS Antenna System (AntS), including solar panels,…
A non-pyrotechnic pin puller utilizing Shape Memory Alloy (SMA) wire, offering a 100 lbf (445 N) pull force…
Quad-link multi-band MilSatCom terminal connecting simultaneously to four satellites across Ka, Ku, and L-band in GEO, MEO, and…
TY-Space Technology offers Star Simulators, including Optical Star Pattern Simulators and Dynamic Star Simulators (DSS-14, DSS-25), designed for…
Complete bidirectional S/UHF/L-band telemetry and communication system for suborbital rockets, including conformal wraparound antennas, SDR transceivers, mobile tracking…
Lightweight GPS L1 patch antenna qualified for space applications.
Satellite constellation digital twin emulator specialized for optical communications mission planning, validation, and operational simulation.
Customized air bearing systems for satellite ADCS testing — used in ground-test rigs such as TU Berlin's TechnoSat…
The ZAPHOD CubeSat Structure range offers lightweight, robust, and user-friendly structures for CubeSats, available in 3U, 6U, and…
L3Harris Technologies is a US defense technology company providing space systems, communication electronics, and space propulsion. L3Harris (formed…
An indoor GaN DBS SSPA/BUC available in 200W, 300W, or 550W output power, featuring a hot-swappable redundant power…
The Intellian C200L is a fixed satellite communication terminal designed for land-based applications, utilizing the Iridium Certus L-band…
A GaAs solar panel with a built-in electromagnetic detumbling coil, sized for CubeSat side surfaces (SXC-SGS-03).
Multi-layer vacuum superinsulation line for cryogenic applications, laser-cut to shape, with polyester, aluminium-foil, LOX-compatible and tape variants.
High-precision chemical thruster with closed-loop pressure control, 20-200 N thrust range.
Self-redundant cosine sun sensor, 160×160° FOV, ±3° OBC-limited accuracy, 15 g ultralight, 0 W passive, >100 kRad TID.
Hydrazine monopropellant engine family from 0.02 lbf to 700 lbf thrust, with more than 19,000 units delivered.
The SP2X is a solar panel designed for 2U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells…
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