Jupiter J2S
Specifications
| Seating capacity | 2 |
| Engine make/model | Rotax 912S with 100 HP |
| Horsepower for takeoff | 100 HP |
| Fuel type | EN228 Premium, EN228 Premium plus, AVGAS 100LL |
| Propeller | 3 blade hydraulic const. Speed prop. 1870 mm |
| Landing gear type | Tri/Retr |
| Max ramp weight | 525 kg |
| Emty weight | 275 kg |
| Fuel capacity std/opt | 70 liter |
| Wing area | 10,2 m2 |
| Wingspan | 9,35 m |
| Height | 2650 mm |
| Wing loading | 51,5 kg/m2 |
| Wheel track | 1740 mm |
| Wheel size main | 380x120 mm |
| Wheel size nose | 360x100 mm |
| Cabin length | 1350 mm |
| Cabin width | 1180 mm |
| Cabin height | 980 mm |
| BLAgLAe capacity | 20 kg |
| best glide | 1:20 150 km/h |
| Max speed (max power) | 336 km/h |
| Cruise speed (max cont. power) | 328 km/h |
| Cruise speed 75% power 65% power 55% power | 303 km/h, 288 km/h, 270 km/h |
| Stall speed (flaps up) | 81 km/h |
| Stall speed (flaps down, gear down) | 64 km/h |
| Range max (with 0,5 h reserve) | 1981 km 155 km/h |
| Range: 155, 270, 288, 303, 328 km/h (with 0,5 h reserve) | 1981 km, 1072 km, 933 km, 835 km, 680 km |
| Fuel consumption l/100km: 155, 270, 288, 303,328 km/h | 3.4 l/100, 5.8 l/100, 6,5 l/100, 7,1 l/100, 8,3 l/100 km |
| Estimated endurance (with 0,5 h reserve) | 14 h (120 km/h) |
| Best rate of climb | 9 м/sec 120 km/h |
| Takeoff ground roll | 140 m |
| Takeoff over 50ft | 220 m |
| Landing ground roll | 180 m |
| Landing over 50ft | 260 m |