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| Typenumber |
V.25. |
Type of aircraft |
Fighter |
| Country |
Germany |
| Date first flight |
1918 |
| Crew |
1 |
| Enginetype |
Oberursel UR.II |
Engine
power |
110hp |
| Wingspan |
8.73m |
| Wingarea |
11.12 m2 |
| Lenght |
5.93m |
| Height: |
2.63m |
| Empty Weight |
384 kg |
| Max. weight |
564 kg |
| Number built |
1 |
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The V.25 was a single seat monoplane fighter with cantilever low-wing developed in parallel with the Fokker V.23.
It had a low-set wing, which improved the view from the cockpit, and was a bit smaller.
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The Oberursel rotary engine was now considered insufficiently powerful, and the V.25 was abandoned.
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