PUL-10
The PUL-10 is a two-seat flying wing - light aircraft , which under the supervision of aircraft designer Reimar Horten was developed. It became the developer's last model. The design was produced in three individual copies by the company Nurflügel Flugzeugbau . The first molded parts were manufactured in 1992.
There were a total of three stages of development of the model. Versions II and III had a Rotax engine that was increased from 54 to 81 hp and a retractable landing gear compared to version I. With each model, the curb weight has been reduced and the speed and range increased at the same time.
The predecessor is the PUL-9 and the successor is the HX-2 .
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| passenger | 1 |
| span | 10.00 m |
| Wing area | 15.42 m² |
| length | 3.96 m |
| height | 1.43 m |
| Empty mass | 369 kg |
| Top speed | 240 km / h |
| Minimum speed | 70 km / h |
| Rate of climb | approx. 5 m / s |
| Summit height | 4000 m |
| Range | 1200 km |
Web links
- PUL-10, the last Horten project (English), flying wing aircraft construction
- Maiden flight of the PUL-10 III in 1997 at the Breitscheid airfield
- Hoarding website