A new ANG 01 aircraft has been designed and manufactured in 2019. ANG 01 is based on the concept of LA-50 aircraft, At the same time, ANG 01 is substantially more perfect than its predecessor. Thus, due the use of new carbon fiber materials, its weight was reduced and its strength characteristics were enhanced. Owing to the usage of specialized computer programs, the company specialists have managed to implement an optimum structure of the fuselage and wing, having achieved hereby their best performance. We have also used the advanced products for computer-based wind-tunnel simulation that allows modeling the characteristics of the airframe and fine-tuning them at the development phase. The development of the aircraft was performed, based on the latest technological achievements, with the use of the up-to-date CAD systems for aircraft design computing, which allowed to carry out the design strength aerodynamics testing, etc. with high precision directly in the computer. Due to the calculations solely in CAD systems, we have obtained the aircraft empty weight of 380-400 kg (maximum configuration), while the maximum take-off weight is of 950 kg. Thus, the payload is 550-570 kg, that is 137%-150% of its own weight. Besides, to enhance the safety of the aircraft, it was equipped with a modern parachute rescue system GRS 6 800-990 SDS manufactured by the Czech company Galaxy GRS s.r.o. Reliability and ease of control is provided by modern electronic SkyView HDX system manufactured by Dynon Avionics. Specifications Number of Seats 5 Engine Rotax 915 iS3A 141 HP fuel Type Avgas A-92, A-95, A-98, 100LL Propeller 3 blade, Variable Pitch Type Landing Gear trycicle type, hydraulically retractable Maximum Takeoff Weight 950 kg empty weight 380 kg The capacityof fuel tanks 245 l wing area 11,3 m2 Wingspan 9,6 m Aircraft Length 7,138 m Height 2,65 m fuselage width MAX 1,35 m cabin height 1,2 m Cabin length MAX 2.3 m Wing loading 84 kg/m2 Landing Gear Tread 1.9 m wheel size 8â?? (420 mm) Luggage Compartment Capacity 780 liters Maximum Lift-to-Drag Ratio 18.6 Max speed 360 km/h Maximum cruising speed 345 km/h Cruising speed 85% 310 km/h landing speed 70 km/h Cruising speed 65% 290 km/h rate of climb 3,5 m/s Takeoff Run 300 m Landing Roll 150 m at an altitude of 4000m Climb rate 8.3m / sec
Airbus A310 Passengers : 218 – 240 Range : 6.800 – 9.630 km Speed : 850 kmh Airbus A320 Passengers : 150 – 180 Range : 4.800 – 6.150 km Speed : 891 kmh Light Jets Cessna Citation Jet C525 Passengers: 4 – 5 Range : 2.400 – 3.700 km Speed : 720 – 839 kmh Cabin (L) : 3,35 – 5,28 m Cabin (H) : 1,45 m Lavatory : yes
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