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Drone Interceptor

Birotor Coaxial High Capacity Helicopter

ALL OUR DEVICES HAVE LANDING CAPACITY AND VERTICAL TAKEOFF (VTOL)

After taking these steps, we are faced with the possibility of designing and building a 6-blade coaxial twin-engine RPA helicopter  for civil and military purposes, which has a greater operating capacity in RANK and MTOW, of any other existing model.

It is for this reason that we developed  our  RPA  helicopter  following this idea and equipped it with  diferente  engine combinatioms – 2 rotary engines or one 160 hp four cylinders  engine … etc… and 3 blades per each rotor

A tail rotor typically wastes some of the available engine power that would be fully dedicated to lift and thrust with a coaxial design. Reduced noise is a second advantage of the configuration; some of the loud “slapping” noise associated with conventional helicopters arises from interaction between the airflows from the main and tail rotors, which in some designs can be severe.

Also, helicopters using coaxial rotors tend to be more compact (with a smaller footprint on the ground), though at the price of increased height , and consequently have uses in areas where space is a priority; The Bi-Rotor Coaxial design is ideal for naval roles, being capable of operating from confined spaces on the decks of smaller ships.

Prototypes Drone Design
RPA
Drone UAV
Birotor Coaxial High Capacity Helicopter
RPA HELICOPTER PROTOTYPE

Our birotor coaxial helicopter allows you to work in different configurations to perform different missions.

Variable Configuration Uav
Autonomous Take-off And Landing System
Prototypes Drone Design
High Range From Civil To Military Applications
Autopilot
Drone Intercepto
FINITE ELEMENTS SIMULATION

Every single component of the helicopter is subjected to a finite element analysis that determines, optimizes and validates the design, strength and durability of each piece.

RPA
GENERAL CHARACTERISTICS

Our birotor coaxial helicopter allows you to work in different configurations to perform different missions.

No tail rotor Helicopter.
Bi rotor coaxial Helicopter.
2 Rotors 3 blades each one.
Coaxial against rotary.
Engines (water cooled).

Possibility.

1 – using 2 Wankel rotary carburation engines.
2 – using 1 engine 3 cylinders fuel injection.
2 – using 1 engine with 4 cylinders fuel injection.

ADJUSTABLE to different configurations according to the combination of needs for flight time and pay-load. Autonomy according to the configuration adopted 2/4/6 hours.

UAV
Drone UAV
Birotor Coaxial High Capacity Helicopter
RPA
Main Specifications
MAIN ROTOR DIAMETER 4420 mm
TOTAL LENGTH 4612 mm
TOTAL HEIGHT 200-245 kg
MTO WEIGHT 4612 mm
PAYLOAD CAPACITY +90 kg
FUEL (INTERNAL TANKS) 40 l , up to 80 l
POWER PLANT 76 hp (2x38hp rotary engines)
OTHER  ENGINES IN OPTION
MAXIMUM SPEED 200 km/h
ENDURANCE 2/4/6/ hours
SERVICE CEILING 12,000 ft
OPERATING TEMPERATURE  -30ºC TO + 57ºC
DATA LINK RANGE Up to 100 – 200 Km
Birotor Coaxial High Capacity Helicopter
Drone UAV