Yakovlev Yak-9P
| GENERAL DATA | |||
| Other Designation(s) | Frank
(NATO) |
||
| Type | Fighter |
Crew | 1 |
| Manufacturer(s) | Plant No.153
(Novosibirsk), Plant No.166 (Omsk), Plant No.82 (Moscow) |
||
| Production | 16769 all-versions
(September 1942 – December 1948) |
||
| First Flight | ? |
Introduction | 1947 |
| Variants | |||
| Yak-9P | Designation reused for an all-metal version of the Yak-9U with a VK-107 engine. | ||
| DIMENSIONS | |||
| Length | 8.55 m |
Empty Weight | 2708 kg |
| Wingspan | 9.74 m |
Loaded Weight | 3550 kg |
| Height | 3 m |
Max takeoff weight | ? kg |
| Wing area | 17.15 m² |
Wing Loading | 207 kg/m² |
| ARMAMENT | ||||
| Main Guns | Engine mounted* |
1 × 20 mm (0.8 in) ShVAK cannon
(final) |
Ammunition Carried | 1x 120 |
| Secondary Guns | Nose ** |
2 x 12.7 mm (0.50 in) Berezin UBS MG |
Ammunition Carried | 2 x 200 |
| Other Armament | - |
|||
(*) firing through propeller hub, (**) synchronized in the upper nose fuselage
| POWERPLANT | |||
| Engine | 1 × VK-107A |
Type & Displacement | V-12 supercharged liquid-cooled,
35.08 L |
| Horsepower (maximum) | 1500
hp |
Power/Weight Ratio | 422.53 hp / ton * |
| Fuel Capacity | 650 L
|
||
(*) with loaded weight
| mPERFORMANCES | |||
| Maximum Speed | 590 km/h at sea level, 550 km/h
at altitude |
Cruise Speed | 304 km/h |
| Stall Speed (takeoff/landing) * | 140 km/h |
Service Ceiling | 10500 m |
| Rate of Climb | 16.3m/s |
Range | 1130 km |
(*) vitesse de décrochage (décollage/atterrissage)
| Sources | |||
| Wikipédia | aviationsmilitaires.net | ||
