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Subject Item
dbpedia:Convair_XFY_Pogo
rdfs:comment
The Convair XFY Pogo tailsitter was an experiment in vertical takeoff and landing. The Pogo had delta wings and three-bladed contra-rotating propellers powered by a 5,500 hp (4,100 kW) Allison YT40-A-16 turboprop engine. It was intended to be a high-performance fighter aircraft capable of operating from small warships. Landing the XFY-1 was difficult, as the pilot had to look over his shoulder while carefully working the throttle to land.
dbpedia-owl:manufacturer
dbpedia:Convair
dbpedia-owl:numberBuilt
3
dbpedia-owl:productionEndYear
1954-01-01Z
dbpedia-owl:productionStartYear
1954-01-01Z
dbpedia-owl:type
dbpedia:VTOL