VTOL aicraft able to fly in all directions having the same aerodynamic characteristics
HIGH LIFT/DRAG RATIO • WIDE RANGE OF USEFUL INCIDENCE ANGLES (EVEN OVER 60 DEGREES) • UNIFORM DISTRIBUTION OF AERODYNAMIC LOAD • NO STAGNATION POINT • NO SHOCK WAVE ON THE SURFACE DURING THE TRANSONIC FLIGHT • NO SONIC BOOM • LOW VIBRATIONS • LOW AERODYNAMIC NOISE • LOW HEATING • REDUCED DRAG IN THE TRANSONIC FLIGHT • HIGH FUEL ECONOMY AT HIGH SPEEDS
• NO JUMP OF PITCHING MOMENT AND NO LIFT FLUCTUATIONS AT TRANSONIC SPEEDS
SMOOTH TRANSITION FROM SUBSONIC TO SUPERSONIC FLIGHT
VTOL • VECTORED NOZZLES FOR CRUISE MANEUVERS (YAW, ROLL AND PITCH)
• REACTION CONTROL SYSTEM - LATERAL AND VERTICAL NOZZLES
• SUDDEN LATERAL TRANSLATIONS AND SUDDEN YAW
• COMBINED MANEUVERS IN ANY DIRECTION AT HIGH SPEEDS
THE ONLY LIMIT OF MANEUVRABILITY IS THE PILOT’S IMAGINATION
PRIVATE AIRCRAFT • UAV • UCAV • FIGHTER AIRCRAFT • MISSILES
STEALTH CAPABILITIES
WO2017105266A1 - patent pending