Yak-25RV Mandrake
| Yak-25RV Mandrake Specifications | ||
|---|---|---|
| Country of Origin | Russia | |
| Builder | Yakovlev | First Flight | 1959 |
| crew | 1 | |
| span | 23.4 meters | |
| length | 15.93 | |
| height | no data | |
| weight | 9,000 kg | |
| Empty weight | 6 175 kg | |
| takeoff weight | 9 800 kg | |
| Maximum weight | no data | |
| load mass | none | |
| engine | Two R-11B-300 | |
| max speed | Speed 870 km/h | |
| ceiling | 21,000 meters | |
| landing run | ||
| range | 3,900km | |
| radius of action | km 3 500 | |
| armament | absent | |
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