RAF2000 Specifications
RAF2000 FI EJ2.2 EXTERIOR
DIMENSIONS
Lenght |
4.15 meter |
Height |
2.59 meter |
Width |
1.53 meter |
Aircraft Dry Weight |
358 Kg |
Payload |
331Kg |
Gross Weight can be set as high as Category Weight |
698.54 Kg |
ENGINE
Manufacturer |
SUBARU |
Displacement |
2200 cc |
Horsepower |
130 hp |
Cooling |
Liquid Cooled |
Ignition |
Electronic, Computer Controlled, Single Spark Plug/Cylinder |
REDUCTION DRIVE
Manufacturer |
RAF |
Type |
HTD COG BELT |
Ratio |
2.10 to 1 |
PROPELLER
Manufacturer |
WARPDRIVE |
# of blades |
3 |
Diameter |
172.72 cm / 68 inches |
Pitch |
Ground Adjustable |
ROTOR BLADE
Manufacturer |
RAF |
Rotor Span |
9.14 M /30 FT |
Blade Cord |
21.56 CM / 8.5 Inches |
Materials |
Composites, Aluminum Spar, Foam Core |
ACTUAL DISC LOADING
Take-off Weight when set at Category Weight | 0.95 Kg / 2.18 LBS/sq.feet |
FUEL CAPACITY
FUEL CAPACITY |
85 Litre / 25 US Gallons |
Endurance (1/2hr on reserve) |
4.6 Hours |
Fuel Consumption (80% or 4200 rpm) |
21.82 Litre per hour / 4.8 US Gallons |
Unusable Fuel |
2.27 Litre / 1/2 Gallon |
Approved Fuel |
Premium Auto Gas / Unleaded |
Grades |
91-93 Octane |
PERFORMANCE
PERFORMANCE |
2.2 FI |
Minimum Speed (Min Altitude 300 FT) |
20-25 mph |
Cruise Speed |
70-80 mph |
Recommended VNE |
100 mph |
Maximum Speed |
120 mph |
Stall Speed |
N/A |
Take-off Air Speed |
30-35 mph |
Take-off Roll (Single Occupant) |
0-75 feet |
Landing Roll |
0-10 feet |
Rate of Climb |
1200 RPM |
RAF2000 FI EJ2.5 EXTERIOR
DIMENSIONS
Lenght |
4.15 meter |
Height |
2.59 meter |
Width |
1.53 meter |
Aircraft Dry Weight |
367 Kg |
Payload |
349Kg |
Gross Weight can be set as high as Category Weight |
698.54 Kg |
ENGINE
Manufacturer |
SUBARU |
Displacement |
2500 cc |
Horsepower |
165 hp |
Cooling |
Liquid Cooled |
Ignition |
Electronic, Computer Controlled, Single Spark Plug/Cylinder |
REDUCTION DRIVE
Manufacturer |
RAF |
Type |
HTD COG BELT |
Ratio |
2.10 to 1 |
PROPELLER
Manufacturer |
WARPDRIVE |
# of blades |
4 |
Diameter |
167.64 cm / 66 inches |
Pitch |
Ground Adjustable |
ROTOR BLADE
Manufacturer |
RAF |
Rotor Span |
9.14 M /30 FT |
Blade Cord |
21.56 CM / 8.5 Inches |
Materials |
Composites, Aluminum Spar, Foam Core |
ACTUAL DISC LOADING
Take-off Weight when set at Category Weight | 0.95 Kg / 2.18 LBS/sq.feet |
FUEL CAPACITY
FUEL CAPACITY |
85 Litre / 25 US Gallons |
Endurance (1/2hr on reserve) |
3.3 Hours |
Fuel Consumption (80% or 4200 rpm) |
25 Litre per hour / 6.5 US Gallons |
Unusable Fuel |
2.27 Litre / 1/2 Gallon |
Approved Fuel |
Premium Auto Gas / Unleaded |
Grades |
91-93 Octane |
PERFORMANCE
PERFORMANCE |
2.5 FI |
Minimum Speed (Min Altitude 300 FT) |
20-25 mph |
Cruise Speed |
90 mph |
Recommended VNE |
100 mph |
Maximum Speed |
140 mph |
Stall Speed |
N/A |
Take-off Air Speed |
30-35 mph |
Take-off Roll (Single Occupant) |
0-75 feet |
Landing Roll |
0-10 feet |
Rate of Climb |
1200 RPM |
NOTES:
* Performance optimum at sea level and dependant on wind
* RAF 2000 Gyroplane requires flight instruction (min of 45hrs in-flight training)
* Prices and specs subject to change without prior notice