| Alpha Electro | |
| Motor |
electric motor |
| power | 50+ KW at 2100 – 2400 rpm |
| PROPELLER | Ground adjustable three-blade 1,65 m diameter propeller |
| PROPORTIONS | |
| wing span | 34,4 ft (10,5 m) |
| length | 21.33 ft (6.5 m) |
| height | 6.07 ft (2.05 m) |
| wing area | 102.4 sqft (9.51 m2) |
| rudder area | 11.8 sq.ft (1.1 m2) |
| horizontal tail area | 11.6 sq.ft (1.08 m2) |
| aspect ratio | 11,3 |
| positive flaps | 0°, 15°, 25° |
| center of gravity | 20% – 38% MAC |
| WEIGHTS | |
| empty weight (with batteries) | 350 kg |
| max take off weight (MTOW) | 550 kg (1212 lb) |
| Payload | 200 kg |
| PERFORMANCES | DATA PUBLISHED FOR MTOW 1,212 lbs (550 kg) All speeds in Knots |
| stall with flaps | 42 KCAS |
| stall without flaps | 45 KCAS |
| VNE | 135 KIAS |
| max. speed with flaps down | 70 KIAS |
| maneouvring speed | 86 KIAS |
| best climb speed | 65 kts |
| max climb rate | 1,220 fpm |
| best glide ratio speed | 64 KIAS |
| best glide | 15:1 |
| take off run MTOW | 492 feet (150 m) |
| take off over 50′ obstacle MTOW | 885 feet (270 m) |
| 45°-45° roll time | 2.6 sec |
| endurance | up to 60 min (+ reserve) |
| max load factor permitted (x1,8) | +4g -2g |
| design safety factors & tested | minimum 1.875 |
Pipistrel reserves the right to revise the above data whenever occasioned by product improvement, government/authority regulations or other good cause.
The design basis follow the strictest EASA CS-22, CS-VLA and CS-23 (sections), as well as rules applicable to ultralight/microlight aircraft (LTF-UL 2003, etc.) and ASTM-LSA standards.
Ultralight/Microlight certification basis varies from country to country, therefore the actual certificated data may be different from stated above. Please check the certifications link.
