Vehicles
제품 상세보기
Alpha Trainer
- File 1
- Price List
- File 2
- Technical Data
ENGINE : ROTAX 912 UL
max power(with 2 carb.) : 80 hp at 5800 rpm
PROPELLER : Fixed pitch wooden 63"/ 1620 mm diameter propeller with protected leading edge
wing span : 34,4 ft (10,5 m)
length : 21.33 ft (6.5 m)
height : 6.07 ft (2.05 m)
wing area : 96.6 sq.ft (9.51 m2)
rudder area : 11.8 sq.ft (1.1 m2)
tail area : 11.6 sq.ft (1.08 m2)
aspect ratio : 11,3
positive flaps : 0°, 15°, 25°
center of gravity: 20% - 38% MAC
empty weight : 615 lbs (279 kg)
max take off weight (MTOW) : 1212 lbs (550 kg)
Payload with full fuel : 507 lbs (230 kg)
fuel tanks capacity : 13,2 US gal (50 l)
useful fuel : 12,7 US gal (48 l)
DATA PUBLISHED FOR TOM of 472.5 kg, all speeds in Knots
stall with flaps : 37 kts
stall without flaps : 43 kts
cruising speed (75% power) : 108 kts
max. horizontal speed : 120 kts
VNE : 135 kts
max speed with flaps down : 70 kts
manoeuvring speed : 86 kts
best climb speed : 75 kts
max climb rate ( 450 kg) : 1,220 fpm
best glide ratio speed : 64 kts
best glide (prop. 90 deg.) : 15:1
take off run ( 450 kg) : 459 feet
take off over 15 m obstacle (450 kg) : 738 feet
service ceiling ( 450 kg) : 18,000 feet
45° - 45° roll time : 2,6 sec
fuel consum. at cruis. speed : 3.6 US gph (13.6 lph)
endurance (std tanks) : 3,1 hours
range distance : 324 NM (600 km)
max load factor permitted ( x 1,8) : +4 g - 2 g
design safety factors & tested : minimum 1.875
