Air
Complete propulsion stacks for Group 1 through Group 3 UAS: motor, ESC, flight controller, and GPS from a single U.S. source.
For aerial platforms
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Platforms
Group 1 to 3 UAS, VTOL, fixed wing, FPV, and ISR platforms.
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Components today
The H7 Pro flight controller, 80A PRO 4-in-1 ESC, SAM-M10 GPS module, and 2-in-1 LED module are in the store now, on pre-order.
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Larger airframes
Low acoustic and EM signature slotless motors for ISR missions, HV bus support to 400+ V for hybrid Group 3 systems, and seal-less pumps for onboard fuel transfer and payload cooling.
UAS group coverage
| Parameter | Group 1 (up to 20 lb) | Group 2 (21 to 55 lb) | Group 3 (up to 1,320 lb) |
|---|---|---|---|
| Class context | Below 1,200 ft AGL, under 100 kts | Below 3,500 ft AGL, under 250 kts | Below 18,000 ft MSL, under 250 kts |
| RPM range | 4,000 to 30,000 | 2,000 to 8,000 | 1,500 to 6,000 |
| Power range | 0.05 to 1.5 kW | 1 to 6 kW | 5 to 50+ kW (system 30 to 150+ kW) |
| Motor size (stator OD) | ~13 to 50 mm (e.g. 1306 to 5010) | ~50 to 90 mm (e.g. 6012 to 8016) | ~90 to 200+ mm |
| Voltage | 3S to 8S (11.1 to 33.6 V) | 6S to 14S (22.2 to 52 V) | 14S to 24S (52 to 100 V), HV bus 270 to 400+ V on hybrid |
| Battery | 4S to 6S LiPo/Li-ion, ~20 to 350 Wh | 6S to 14S Li-ion, ~0.5 to 3 kWh | HV packs, multi-kWh to tens of kWh, often hybrid generator plus buffer |
Standard configurations within these ranges are sold commercially off the shelf. Parameters reflect current platform capability ranges. Application-specific performance data, including duty cycle and environmental qualification, is available under NDA and co-developed to program requirements.
Build a propulsion stack
Tell us the airframe, group, and mission, and we'll put together the motor, ESC, flight controller, and GPS.