|Wing Load (kg/m2)||70.0|
|Power load (kg/hp)||9.8|
|Speed at 0m||220km/h|
One of first general purpose aircraft built in the USSR. Following roles were suggested for the G-21:
Clean low-wing cantilever monoplane with fixed landing gear and enclosed 2-3 seat cockpit. Leading edge automatic slats were synchronized by steel tube running through the fuselage. Typical for V.K.Gribovskij aircraft stressed skin wooden construction - 2mm plywood monocoque fuselage, wing covered by plywood from the leading edge to the second spar, after the second spar - fabric.
G-21 easily passed all trials, used later for training.
|Created January 6, 1999||Back to|