TeST ATLAS 10

 

BRAND and MODEL

TeST ATLAS 10

TYPE

Two-seat self-launched glider

ORIGIN

Czech Republic

ENGINE

One 30 kw (40 hp) Rotax 447UL2V two-cylinder, two-stroke, fan-cooled engine with electronic single ignition

SPECIFICATIONS 

Wingspan: 15 m (49 ft 2 in)

Length: 6.87 m (22 ft 6 in)

Wing area: 9.85 m² (106 sq ft)

Max manoeuvring speed: 140 km/h (87 mph)

Cruising speed: 105 km/h (65 mph)

Stalling speed: 61 km/h (38 mph)

Service ceiling: 2,438 m (8,000 ft)

Rate of climb: 183 m/min (600 ft/min)

Glide ratio 40 at: 88 km/h (55 mph)

Take-off distance over 15 m (50 ft) obstacle: 360 m (1,180 ft)

Landing distance over 15 m (50 ft) obstacle: 230 m (750 ft)

Empty weight: 285 kg (628 lb)

Loaded weight: 435 kg (959 lb)