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RAINBOW AIRCRAFT Ltd. |
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Cheetah |
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Specifications ROTAX
582 ROTAX
912 ROTAX
912S Empty
Weight Gross
Weight Useful
Load Load
Factors +6g -4g +6g -4g +6g -4g Wing span Wing Area Chord Aspect
Ratio 7.01 7.01 7.01 Aircraft
Length Aircraft
Height (at Wing) Cockpit
Height Cockpit
Width Headroom ~850 mm ~850 mm ~850 mm Legroom ~1100 mm ~1100 mm ~1100 mm Seats 2 2 2 Luggage
Compartment 2 x 25L 2 x 25L 2 x 25L Fuel
Capacity 100L /
26gal 100L /
26gal 100L /
26gal Doors
(optional) 2 * 2 * 2 * Power
Plant Engine 582 /99
UL 912 UL 912 ULS Output 65 HP 80 HP 100 HP Gearbox
reduction 3.47 : 1 2.27 : 1 2.27 : 1 Propeller 2/3*
Blade 2/3*
Blade 2/3*
Blade Fuel
Consumption (at 80%) ~14.5
l/hr ~12 l/hr ~13 l/hr Performance
at sea level at MAUW with doors on Take Off
roll Landing
Ground Roll Rate of
Climb 700
ft/min 730
ft/min 900
ft/min Service
Ceiling Max
crosswind component Cruise
Speed (at 65%) Maximum
level Speed 100 mp/h Max Speed
(VNE) Glide
Ratio ~10 : 1 ~10 : 1 ~10 : 1 Power Off
Stall (with No flaps) Power Off
Stall (with flaps) Roll Rate ~3 sec
45/45 ~3 sec
45/45 ~3 sec
45/45 Endurance
(with reserve) ~6.5 hrs ~7.5 hrs ~7.0 hrs Range
(with reserve) ~500 miles ~670 miles ~700 miles |