A modular, lightweight GaN-based PPCU platform, not a catalogue — the envelopes below are design targets we will freeze with early integration partners, informed by the team's silicon ZVZCS flight-programme heritage and today's silicon breadboard.
50–500 W Hall and cathode-heater systems on small satellites — the volume end of the constellation market.
1–2 kW for LEO station-keeping and orbit topping — the workhorse class, and the first engineering model we build.
5 kW+ for orbit raising and all-electric buses — where the team's 6.5 kW heritage lives.
| Envelope | Target | Basis | Status |
|---|---|---|---|
| Power classes | ~0.05–0.5 / 1–2 / 5+ kW | Market classes served by merchant PPUs today | Design target |
| Discharge topology | Resonant soft-switched · wide-bandgap GaN | Carried from team ZVZCS heritage at 6.5 kW / 90% (ISRO programme, silicon) | Silicon breadboard running · GaN EM in design |
| Efficiency | >90% class goal | Heritage-derived; to be evidenced per class | To be measured on EM |
| Mass | Substantially lighter per kW than legacy silicon units | Magnetics shrink with switching frequency (GaN) | To be evidenced on EM |
| Outputs | Discharge · heater · keeper · magnets · housekeeping | Standard Hall-system complement | Architecture frozen at EM design |
| Control | FPGA sequencing, protection, telemetry | Team background in high-rel embedded/FPGA | In design |
Not a procurement datasheet — target envelopes for integration discussions, updated as test gates are passed.