Safe training gliders, with independent takeoff and landing on various sites (asphalt, ground, etc.)
Presented by models:
With turbojet engines
«Skyline Solo Jet» - ultralight single seat jet glider
«Skyline Solo Screw Motor» - ultralight two-seater glider
With electric propeller motors
«Skyline Twin Jet» - ultralight single seat jet glider
«Skyline Twin Screw Motor» - ultralight two-seater glider
Glider "Skyline Solo Jet" with jet engines, single
Weight 115 kg (+ fuel), two turbines (jet engines) with a thrust of 30 kg. Takeoff distance 120 meters (this is over a field with grass, less than 100m on asphalt). Rate of climb 8 m / s. The fuel consumption is 1 liter per minute for each turbine (2 liters per minute for 2 turbines).
Can fly (and take off) on one engine, in this case the climb rate is 2.5-3 m / s
The maximum speed is 220 km / h.
Stall speed 75 km / h
It is possible to install additional fuel tanks in the wings - flights over 400 km become possible.
The quality of the glider with the engine retracted - 32 (at a speed of about 100 km.h when gliding) - this is an average characteristic, but not very bad for an educational and recreational glider, it means how long the glider will fly when rising to a height equal to one, without using ascending currents, the engines are used usually only for climbing to a height from which stable flows begin (this rises about a kilometer in 2-2.5 minutes.
At a regular refueling, 30 liters rises to a height of 6 km, but for heights above 3.5 km, you need to reconfigure the engine (this is fast).
At the moment, variants of the airframe are being manufactured based on a composite of fiberglass, and a composite of carbon (increases strength characteristics and tolerances for maximum overloads). It is also planned to introduce composites using nanotubes to increase the strength and dynamic characteristics, which has not yet been introduced throughout the world.
The Skyline Solo Jet was designed to meet the specifications of the FAI International Glider Committee for the World Class Glider competition.
The gliders are registered with the Federal Aviation Administration (US Department of Transportation) REGISTRY, (Manufacturer Name Entered: AVIASTROITEL) and are used extensively in US flight schools.
Thanks to the high quality of production, attention to detail and focus on European standards, the reliability and modernity of our gliders allows us to set world records.
Reliable certified glider, very economical and comfortable air vehicle. Simplicity and ease of use and transportation of the glider. The glider is the most affordable closed cockpit aircraft and the most eco-friendly fast vehicle!
Flight weight: 260 kg
Tank volume: 40 l
Startup and exit time: about 1.5 minutes
Launching in the air is possible up to an altitude of 2500 m at a speed of 100-120 km / h
Average fuel consumption when climbing 800-900 m: 8 l
Maximum rate of climb: 8 m / s
Maximum takeoff weight: 260 kg (573 lb)
Maximum payload: 120 kg (265 lb)
Operating overload range + 5.3 / -2.65
Wing loading with a flight weight of 260 kg: 30 kg / m2; 6.15 f / f2
Number of pilots: 1Maximum aerodynamic quality speed: 95 km / h; miles / hour 59; knots 51
Rate of vertical descent at maximum quality: m / s 0.805; ft / min 150
Maximum permissible speed (Vne): 220 km / h; miles / hour 137; knots 119
Maximum permissible maneuver speed (Va): 160 km / h; miles / hour 99; knots 86
Pre-landing planning speed under normal weather conditions, not less: 100 km / h; miles / hour 60; knots 55
Wingspan 12.6 m; 41.3 feet
Glider length 5.25 m; 17.2 feet
Glider height 1.25 m; 4.1 feet
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