Specifications  
External Dimensions:
  FLIGHT DEPLOYMENT ROAD OPERATIONS
Width 28 ft. 4 in. 8 ft. 6 in.
Length 17 ft 2 in. 14 ft. 5 in.
Height 9 ft. 7 in. 5 ft 8 in.
Wheel Base 8 ft. 11 in. 8 ft. 11 in.
Wing Surface Area:    
Main Wing 119.3 ft.2  
Canard 20.7 ft.2  
Total Area 140.0 ft.2  
Propulsion:
  FLIGHT DEPLOYMENT ROAD OPERATIONS
Powerplants IO-360 or equivalent 1,400 cc, 4 cyl, 4-stroke
Performance 180 hp @ 2,700 rpm 80 hp
Propeller 66 inches, 3 blade, (remains to be optimized)  
 
   
 
Weights and Loadings:
  FLIGHT DEPLOYMENT ROAD OPERATIONS
Empty 1,150 lb. 950 lb.
Useful Load 450 lb. 450 lb.
GTOW 1,600 lb.  
Wing Loading @ GTOW 11.42 lb./ft.2  
 
   
Performance Estimates  
Performance Estimates :
  FLIGHT DEPLOYMENT ROAD OPERATIONS
Maximum Speed @ 3,000 ft.
@ GTOW		 180 kts 100 mph
Cruise Speed 153 kts 65 mph
Stall Speed @ Sea Level 50 kts.  
Range @ 3,000 ft., 130 kts 1,000 nautical miles  
Take-off Distance over 50 ft.3 1,075 ft.  
Landing Distance over 50 ft.3 665 ft.  
 

 

  1. All specifications are design estimates.
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  2. Derived from conceptual design and engineering analysis.
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  3. Listed takeoff and landing distances are calculated using standard aircraft design parameters and do not reflect the use of the vehicle's motorcycle engine and brakes. The use of a separate engine for power directly to the rear wheel, along with increased braking power, will significantly reduce this vehicle's runway distance requirements.