149 satellite platforms, components and ground equipment from manufacturers worldwide.
The Magdrive Warlock is a compact electric propulsion system for CubeSats, utilizing a metal propellant and pulsed power…
The Magdrive Rogue is an integrated electric propulsion system for 2U CubeSats, utilizing a metal propellant and pulsed…
Radioisotope-powered electric thruster delivering 3,048 s specific impulse at only 3 W power draw, targeting small satellite and…
The Jinwu Electric Propulsion System is Hongqing Technology next-generation argon-fueled electric propulsion platform, developed entirely in-house for commercial…
Iodine-fed electric propulsion system family for small satellites, deployers, and OTVs, from 50 W to 150 W.
ExoTerra offers the Iris Propulsion Module, a bolt-on solar electric propulsion system for small spacecraft, and a Propulsion…
High-efficiency electrospray thruster with 3,000 s Isp and 50% mass reduction via aerogel-integrated propellant.
CU Aerospace’s Fiber-Fed Pulsed Plasma Thruster (FPPT) provides very high specific impulse greater than 3,500 seconds via a…
Miniaturized warm-gas resistojet propulsion system for CubeSats with integrated main thruster and 3-axis ACS.
ThrustMe provides advanced in-space propulsion solutions, including iodine-fueled electric propulsion systems, designed for satellite constellations and orbital maneuvering.
Turn-key RF electrodeless plasma propulsion system for 20–500 kg satellites — 5.9 kg dry, 8–18 mN thrust, 600–1,300…
Modular ~1U FEEP electric propulsion unit with 40 individually controlled thrusters and solid metallic propellant, for spacecraft from…
High-Isp electric propulsion ablating spooled PTFE fiber via short pulses — >3,500s Isp, no pressurized tank, scales 0.7L-53L,…
Switching unit routing electrical power between electric propulsion power supplies and thrusters — routes signals from two PPUs…
NASA NIAC-funded nuclear pulsed-plasma propulsion concept aiming to cut crewed Mars transit time to about two months —…
Electric thruster ingesting residual atmospheric particles at Very Low Earth Orbit and converting them to plasma for continuous…
High-thrust water resistojet propulsion for microsatellites in LEO mega-constellations — 75–150 mN thrust and 240 s Isp for…
High-Isp xenon (or krypton) resistojet for geostationary satellite Reaction Control Systems, designed as a non-toxic replacement for hydrazine…
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