Capacity

Empty Weight                                    900 lbs. 

Payload                                              650 lbs, 

Max Take off Gross. Wt.                   1550 lbs.

Fuel Tank                                           12 gal.   ( 72 lbs )

Performance

Cruise Speed                                    170 mph  @ 3000 ft.

Max Speed                                        190 mph.

Vne                                                     220 mph

Dual engines fuel consumption       4 gal / hour. 

Rate of Climb                                    1300 fpm

Service Ceiling                                  10,500 ft.  (15,000 ft With turbo charger )

Hover Ceiling                         9,000 ft

Cruise Duration                                 3 hour  ( 2.5 hours with extra 10 gal fuel tanks )

Range                                                 420 miles  ( 770 mile with extra 10 gal fuel tanks )

 Tandem Rotors system 

Rotary Wing span                             17 ft

Type :                                      Variable Airfoil Tilt Flaps and Slats Anti Oscillation Rotary Wing

Configuration :                                   Straight diameter wings

Rotation RPM hover                         480 RPM

Variable                                             324 RPM @ 190 mph forward flight or   10 %

 Wing Tip Speed                                290 mph @ hover, or    427.2 feet / sec.

Wing Tip Speed                                482 mph @ Max forward flight speed.

                           ( speed of sound  761 mph, 1116 ft /sec )

 Wing ( Blade ) Chord                        20” inch                                                                                     

Wing Area                                          28 sq ft / per rotor

Wing load @ hover average            26 lb/ sq ft,    @ level fly = 30 lb /sq ft

Disc area                                           226.9 sq ft

Autorotation rotor disc load = 3.2 lbs / sq ft.

 Rear Pusher Rotor Assembly – Anti Torque Coaxial Dual Rotors

Rotor diameter                                  66”,   5.5 ft

RPM                                                   0 – 1800 rpm

Structural                                            Coaxial 2 blades x 2 ( Linn’s another patent pending technology )

Collective Pitch Control                    Positive and negative and variable pitch on both coaxial blades

Full RPM Tip speed                          353 mph  Max level flight tip speed =  392 mph

 Power Plant

Engine                                                 600 CC 4 stroke engine (X 2), Water-cooled.

Horsepower                                        70 HP X 2 ( dual ) @ 11,500 RPM ( before using turbo )

Toque                                                  451.3 lbs-inch  (X 2)  

Compression ration                            12:1 

Engine dry weight                               125 lbs

Fuel Injection Type:                             PGM-DSFI Programmed –Dual Stage Fuel Injection

Fuel type:                                            91 Octane gas fuel. or Av Gas, or a combination of both.

Fuel Consumption                              1 gal / hour @  3,500 RPM,