5739 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Qualified 6kW xenon Hall-effect thruster delivering over 359mN thrust and up to 1783s specific impulse for all-electric satellites.
IHI Aerospace flight-proven 22N bipropellant thruster using Hydrazine/NTO with 295s Isp and 583 kg demonstrated propellant throughput.
IHI Aerospace flight-proven 124N bipropellant thruster using MMH/MON3 with 274.9s Isp, 40,000s demonstrated life and 446 kg throughput.
IHI Aerospace flight-proven 50N hydrazine monopropellant thruster with 225s Isp, >14,000 demonstrated pulses and >107 kg throughput.
IHI Aerospace flight-proven 450N bipropellant thruster using Hydrazine/NTO with 326s Isp and 32,850s demonstrated total impulse life.
IHI Aerospace qualification-tested 24.5N hydrazine monopropellant thruster with >7,500 demonstrated pulses, an evolution of the flight-proven MT-2.
IHI Aerospace flight-proven 50N-class hydrazine monopropellant thruster with 23–50N thrust range, >14,800 demonstrated pulses and >120 kg throughput.
IHI Aerospace flight-proven 4N-class hydrazine monopropellant thruster with 1.8–5.0N thrust range, >850,000 demonstrated pulses and >190 kg throughput.
IHI Aerospace flight-proven 20N-class hydrazine monopropellant thruster with 6.9–19.6N thrust, >261,914 demonstrated pulses and >115 kg throughput.
IHI Aerospace flight-proven 0.3–1.1N hydrazine monopropellant thruster with >850,000 demonstrated pulses and >100 kg throughput, heritage on Japanese…
High-sensitivity analog 3-axis magnetometer hybrid in a 20-pin DIP package, using HMC1001/HMC1002 sensors with +/-2 gauss range and…
Economical single-gimbal CMG for small satellites delivering 50 ft-lb-sec momentum and 50 ft-lb peak torque at only 120…
Three-axis smart digital magnetometer with 16-bit resolution, measuring up to 2 gauss with 0.1 milligauss resolution via RS-232/RS-485…
Plug-and-play reaction wheel assembly for small satellites with 11.5 Nms momentum storage, 0.2 Nm reaction torque, and 7-year…
High-output, low-jitter reaction wheel for precision pointing control, up to 1 Nms momentum at 9000 rpm, 1.3 kg…
Plug-and-play reaction wheel assembly for small satellites with 6 Nms momentum storage, 0.2 Nm reaction torque, and 7-year…
PC-104 form-factor CubeSat EPS with super capacitor backup, MPPT, up to 40 W power management, and 3.3V/5V/12V regulated…
Nano/micro satellite platform from Hemeria designed for Earth observation (EO) missions, part of the company's small satellite product…
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