Thruster Control & Drive Electronics for Spacecraft |
Customer: various thrusters
developers under institutional R&D |
Year: 1997 (RMT Project) – ongoing (HPP Projects) |
Main features (HPP): Anode, up to 250 Watt, with remote setup of operating voltage in the range 100÷350 Vdc in steps of 1.5 Vdc, <200 mV ripple, <2 ms transient recovery time; efficiency 79%
Trim Coil, up to 10 Watt on a 0.16 Ω load, for magnetic field intensity control, with:
Ignitor (150 Vdc) / Keeper (22÷24 Vdc), up to 30W
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