Performances in terms of take-off run and climb are equivalent to those of << Rallye 893 >> tow plane
Equipment:
- Airdrop handle between the two seats (yellow).Rearview mirror placed on top of the cabin.
- ROTAX 912ULS (100CV) engine with electric fuel pump
- DUC FLASH propeller (diam. 1850mm)
- Balistic JUNKERS parachute
- BERINGER brakes and wheels (handle on the stick)
- Strengthening of formers 4 and 5 of the fuselage
- The TOST hook is welded on a square 40×40 tube, which is itself fixed on a mesh support welded into square tubes, attached to the steel cabin.
- Mini camera under the fuselage with monitor on the instrument panel.
Build Kit:
- 80% built kits: fuselage, wings, flaps, ailerons, vertical stabilizer, elevator and horizontal stabilizer come assembled
- Plans and instructions included
- Excluded: Engine, propellers, beringer kits, parachute, radios/transponders, spare ruder, and instruments
- 3 year manufactures warranty for the airframe.
1. Performances during take-off and climb while towing a single-seater glider: 376 kg in mass
| Carried out measurements | PEGASE Glider | Observations |
| Runway distance | 190 m | Average of two take-offs |
| Acceleration time | 16 s | |
| Take-off distance (50ft crossing) | 530 m | Light head wind |
| 50ft time lapse | 21 secondes | |
| 1500 ft/ground climb time lapse | 3 min 30 s | Measured after take-off |
| Average variometer | 2.55 m/s | |
| Chosen VTA (flap 0°) | 120 km/h |
2. Performances during take-off and climb while towing a two-seater glider: 600 kg in mass
| Runway distance | 260 m | Temperature on ground: 18° |
| Acceleration time | 19 s | |
| Take-off distance (50ft crossing) | 600 m | |
| 50ft time lapse | 26 seconds | Light head wind |
| 1500 ft/ground climb time lapse | 3 min 50 s | Measured after take-off |
| Average variometer | 2.55 m/s | |
| Chosen VTA (flap 0°) | 120 km/h |
| Reference empty weight | 304.7 kg |
| Wingspan | 9.91 M |
| Useful load | 167.8 kg |
| Load factor | +4/-2 g |
| Wing surface | 14.27 m2 |
| Height | 2.34 m |
| Cabin width | 1.22 m |
| Rate of climb to 1000ft | 1500 feet/min |
| VNE | 200 km/h |
| VNO | 180 km/h |
| VA | 130 km/h |
| VFE (flaps 15°) | 110 km/h |
| VSO | <60 km/h |
| Gliding flight speed (clean configuration) | 100 km/h |
Take-off run with glider : between 188 and 260m
Take-off distance with glider (50 ft height) : 536m (single seater)
Diameter main wheel : 600×6
Diameter front wheel : 500×6
