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The RWD-23 was a Polish low-wing trainer aircraft of 1938 constructed by the RWD team that remained a prototype.

Made by RWD (aircraft manufacturer).

Height Main
1.9 m
Designer
RWD (aircraft manufacturer)
RWD team
Stall Speed Main
65.0
Jet Or Prop
prop
Range Main
450.0
Loaded Weight Main
550.0
Type Of Prop
four-cylinder air-cooled inverted straight engine
Max Speed Main
171.0
Capacity
1.0
Loading Main
34
Cruise Speed Main
150.0
Ceiling Main
3
500 m
Number Built
1
Crew
1
Span Main
11.1 m
Area Main
16 m²
Primary user
Poland
Plane Or Copter?
plane
Power Alt
46.0
Engine(prop)
Walter Mikron II
Manufacturer
RWD (aircraft manufacturer)
Status
prototype
Useful Load Main
225.0
First Flight
1938
Climb Rate Main
2.6 m-s
Power Main
62 hp
Number Of Props
1
Length Main
8 m
Similar Aircraft
*de Havilland Moth Minor - ICAR Universal - Yakovlev UT-2 - Miles Hawk Trainer - CSS-10
Empty Weight Main
325.0
Category
Polish civil trainer aircraft 1930-1939

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