DFS 39d - Project X In 1937, the Research Department of the Air Ministry ordered a tailless aircraft designed
for rocket propulsion. The construction of the aircraft was to be at the Heinkel Aircraft Company in Peenemunde.
Subsequent wind-tunnel testing of the design showed that a central rudder was preferable to the wingtip rudders used in previous designs.
It is obvious from the look of the design of this plane that it is a precursor to the Me 163.
Original schematic with the drooped wingtips |
Later version with the improved central rudder |
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Wind-tunnel testing with the later design. The picture has been inverted, since the testing was done with the model inverted |
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