Tupolev ANT-9 Civil Aircraft Model Details

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General Information of Tupolev ANT-9

Developed Into : Tupolev ANT-14

First Flight : 10714

Introduction : 1931

Manufacturer : Tupolev

National Origin : Soviet Union

Number Built : ~100

Primary Users : Aeroflot

Retired : 1945

Role : Airliner

General characteristics of Tupolev ANT-9

Capacity : 9 passengers

Crew : 2

Empty Weight : 4,400 kg (9,700 lb)

Height : 5 m[3] (16 ft 4¾ in)

Length : 17.01 m (55 ft 9? in)

Loaded_Weight : 6,200 kg (13,668 lb)

Powerplant : 3 × Mikulin M-17 water-cooled V-12, 373 kW (500 hp) each

Wing Area : 84.0 m² (904 ft²)

Wingspan : 23.85 m (78 ft 10 in)

Performance of Tupolev ANT-9

Cruise Speed : 180 km/h (97 kn, 112 mph)

Maximum Speed : 215 km/h (117 kn, 134 mph)

Power/Mass : 0.12 kW/kg (0.073 hp/lb)

Range : 700 km (378 nm, 435 mi)

Rate Of Climb : 2.8 m/s (550 ft/min)

Service Ceiling : 5,100 m (16,732 ft)

Wing Loading : 73.8 kg/m² (15.1 lb/ft²)

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