Convair XFY Pogo
Use attributes for filter ! | |
Top speed | 982 km/h |
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Range | 640 km |
Weight | 5310 (kg) |
Cruise speed | 640 km/h |
First flight | August 1, 1954 |
Engine types | Allison YT40 |
Date of Reg. | |
Date of Upd. | |
ID | 1673560 |
About Convair XFY Pogo
The Convair XFY Pogo was an experiment in vertical takeoff and landing tail-sitter. The Pogo had delta wings and three-bladed contra-rotating propellers powered by a turboprop engine. It was intended to be a high-performance fighter aircraft capable of operating from small warships.