RWD 9 Civil Aircraft Model Details

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General Information of RWD 9

Designer : Stanislaw Rogalski and Jerzy Drzewiecki

First Flight : 12392

Introduction : 1934

Manufacturer : DWL

Number Built : 1 static test, 1 prototype, 8 production

Primary Users : Polish civilian aviation; Czechoslovakia; Spain; France

Produced : 1933-1934

Role : Sport Aircraft

General characteristics of RWD 9

Capacity : Two passengers

Crew : Two, pilot, mechanic

Empty Weight : 560 kg (1,232 lb)

Height : 2.03 m (6 ft 8 in)

Length : 7.6 m (24 ft 11 in)

Loaded_Weight : 790 kg (1,738 lb)

Max Takeoff Weight : 930 kg (1,860 lb)

Powerplant : 1 × GR-760 air-cooled 9-cylinder radial engine, 216 kw (290 hp)

Useful Load : 370 kg (814 kg)

Wing Area : 16.00 m² (172 ft²)

Wingspan : 11.64 m (38 ft 1 in)

Performance of RWD 9

Cruise Speed : 255 km/h (152 knots, 175 mph)

Maximum Speed : 281 km/h

Power/Mass : 3.2 hp/kg ()

Range : 800 km (432 nm, 497 mi)

Rate Of Climb : 6.1 m/s (1,200 ft/m)

Service Ceiling : 7,000 m (22,960 ft)

Stall Speed : <54.1 km/h (29 knots, 33 mph)

Wing Loading : 58 kg/m² (max weight) (11.9 lb/ft²)

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