The RWD 2 was constructed by the RWD team of Stanisław Rogalski, Stanisław Wigura and Jerzy Drzewiecki in the Aviation Section of Mechanic Students' Club of Warsaw University of Technology. It was a development of their first design RWD-1. Its feature was a unique, fish-shaped fuselage, with good aerodynamics, but without a direct view forward from the pilot's seat. For this reason, they were later nicknamed: blind mice. The first prototype was completed and flown by the designer Jerzy Drzewiecki in July 1929. Since it appeared successful in sports flying, three more RWD-2s were built in 1930.
Use
In August–September 1929, Franciszek Żwirko and Stanisław Wigura flew the prototype across Europe, on the 5000 km Warsaw-Paris-Barcelona-Warsaw route. On 16 October, 1929, Żwirko and Antoni Kocjan set an international FAIaltitude record of 4,004 m in the light tourist plane class. Three serialaircraft took part in the Challenge 1930 international touring planes competition in July 1930. Stanisław Płonczyński took the 19th place, as the best Pole, and Edward Więckowski took the 21st place. In the Challenge, RWD-2s won the trial of lowest fuel consumption. According to Flight, they "appear to possess particularly good air-sailing qualities". RWD 2s were also used in several Polish air competitions and other minor international ones, with some success. They were also used for training in the Polish Aero Club in Warsaw, Poznań and Vilnius. They were withdrawn in 1935.
Description
Wooden construction high-wing cantilever monoplane, conventional in layout. Fuselage rectangular in cross-section, plywood covered. Single-spar one-part wing of a trapezoid shape, covered with canvas and plywood in front. Cantilever empennage, covered with plywood and canvas. Crew of two, sitting in tandem, with dual controls. The crew cabs were open on the sides in upper part, they had individual doors on the right side. Salmson 9Ad, 46 hp, 9-cylinder air-cooled radial engine in front, driving a two-bladed metal propeller. Conventional fixed landing gear, sprung by rubber rope, with a rear skid. Fuel tank 75 l in fuselage front.
