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
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Aircraft spare parts.
Aviation Jet Fuel is a type of aviation fuel designed for use in aircraft powered by gas-turbine engines. It is colourless to straw coloured in appearance. The most commonly used fuels for commercial aviation are Jet A and Jet A1, which are produced to a standardised international specification. The only other jet fuel commonly used in civilian turbine-engine powered aviation is Jet B, which is used for its enhanced cold-weather performance. Jet fuel is a mixture of a variety of hydrocarbons. Because the exact composition of jet fuel varies widely based on petroleum source, it is impossible to define jet fuel as a ratio of specific hydrocarbons. Jet fuel is therefore defined as a performance specification rather than a chemical compound. Aviation Jet Fuel is commonly referred to as JP54. However, this is the wrong terminology as there is no such grade of Jet Fuel. Jet A and Jet A1 are what refineries offer. Aviation Jet fuel Gas is what powers turbine aircraft engines. Worldwide, Jet Fuel is the most used low Sulphur content Kerosene. For instance, Colonial JP54 is similar to Jet A except the energy is 18.4 mj/Kg compared to the 42.8 MJ/kg of Jet A. Most importantly there is also a slight difference in additives. Aviation Jet Fuel B is used for its extremely cold weather performance. However, aviation Jet fuel Bs lighter composition makes it more dangerous to handle. For this reason, it is rarely used except in very cold climates. A blend of approximately 30% Kerosene and 70% Gasoline. Because of its very low freezing point (60 C (76 F), it is known as a wide cut fuel and has a low flash point as well. Aviation Jet Fuel B is primarily used in some military aircraft. In Canada, it is also used because of its freezing point. Aviation Kerosene standards are published as GOST10227-86. The standard consists of different properties. It separates paraffin and gasoline in the refinery. Military organisations around the world use a different classification system of JP (for Jet Propellant) numbers. Some are almost identical to their civilian counterparts and differ only by the amounts of a few additives. For instance, Jet A1 is similar to JP 8, Jet B is similar to JP 4. Military fuels are highly specialised products and are developed for very specific applications. Jet fuels are sometimes classified as kerosene or naphtha type. Kerosene type fuels include Jet A, Jet A1, JP 5 and JP 8. Naphthatype jet fuels, sometimes referred to as wide cut Jet Fuel, including Jet B and JP 4.
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