Specification Sheet Data
Seats 2
Passengers 100 kg each
Baggage 50 kg
Endurance 5 hrs Plus 45 mins reserve
Engine 2 * 85 Hp Jabiru 2200 engines
Fuel consumption 16 Litres/hr at 75% power (Jabiru quote
15lts/hr @75%)
15lts/hr @75%)
Preliminary Sizing, Derived Data
MTOW 900 kg 1984 Lbs
Empty Weight 522 kg 1152 Lbs
Payload 250 kg 551 Lbs
Fuel 123 kg 271 Lbs 171 Litres
Wing Span 9 m
Wing Chord 1.3 m
Wing Chord 1.3 m
Aspect ratio A 6.9
Wing Surface (S) 120 sq.ft
Wing Loading (W/S) 16.5 Lbs/sq.ft
Stall Clean (Vs) 59.0 kts (63.6 kts at 5000’)
Stall Flap (Vso) 52.1 kts (56.1 kts at 5000’)
Take off ground roll 51 m (59m at 5000’)
Take off to 50’ 84 m (98m at 5000’)
Landing over 50’ 425 m (493m at 5000’)
Landing roll 219 m (254m at 5000’)
Rate of climb 1710 ft/min (1315 ft/min at 5000’)
Single engine climb 527 ft/min (304 ft/min at 5000’)
Vy 82 kts (88 kts at 5000’)
Vyse 79 kts (85 kts at 5000’)
Vcr at 75% power 123 kts (129 kts at 5000’)
Range at 75% power 600Nm
Range at 75% power 600Nm
Preliminary Design Sequence I, Derived Data
Fuselage Length 6 m
Propeller Sizing
Wing:
Surface Area
Aspect Ratio
Sweep Ratio
Thickness Ratio
Taper Ratio
Incidence angle
Twist angle
Dihedral angle
Aerofoil
Horizontal Tail Surface Area
Vertical Tail Surface Area
Longitudinal Tip-Over angle
Ground clearance angle
Wing tip bank angle clearance
Wheel Tire sizing
C of G range
VMCA
Preliminary Design Sequence II, Derived Data
