Compact classWP-20-23
Entry thrust for small fixed-wing airframes
- Thrust
- 20–23 kgf
- Dry weight
- 3.10 kg
- Max RPM
- 108,000
Engine lineup
Six engines, 20 to 160 kgf
Two compact units, two mid-class and two heavy-class engines, from the 1.74 kg 240A to the 20.88 kg WP160. Figures below are the rated values from each model datasheet.
6 models
Showing 6 of 6 models
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Compact class
Compact class240A
24 kgf in a 1.74 kg engine
- Thrust
- 24 kgf
- Dry weight
- 1.74 kg
- Max RPM
- 116,000
Mid classWP40
Target-drone power with a 4,000 m start ceiling
- Thrust
- ≥40 kgf
- Dry weight
- 4.60 kg
- Max RPM
- 91,500
Mid classWP80
80 kgf for high-speed unmanned aircraft
- Thrust
- ≥80 kgf
- Dry weight
- 10.50 kg
- Max RPM
- 60,200
Heavy classWP120
The first step into heavy-class thrust
- Thrust
- ≥120 kgf
- Dry weight
- 14.50 kg
- Max RPM
- 62,500
Heavy classWP160
Top of the current range
- Thrust
- ≥160 kgf
- Dry weight
- 20.88 kg
- Max RPM
- 46,000
Selection help
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If two classes look close, describe the airframe and target take-off weight. The reply names one model, its limits and the current lead time.
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Figures are rated values from the model datasheets; factory test performance can vary by 2–3%. Final configuration and limits are confirmed in the written quotation. Need a thrust level outside this range? Ask about custom requirements.