Focke-Wulf Fw-190D
GENERAL DATA |
Dora,
Lang Nasen |
High-Altitude
Fighter
|
1 |
Focke-Wulf |
674, ~700
|
Late 1942 |
1944 |
Variants |
Fw 190 D (nicknamed Dora; or Long-Nose Dora ("Langnasen-Dora")
was intended as the high-altitude performance version of the A-series. |
First D-0 prototype was completed in October 1942 with
a supercharged Junkers Jumo 213 including a pressurized cockpit and
other features making them more suitable for high-altitude work |
Initial production |
Initial production |
D-9 series was rarely used against heavy-bomber raids,
as the circumstances of the war in late 1944 meant that fighter-versus-fighter
combat and ground attack missions took priority. This model was the
basis for the follow-on Focke-Wulf Ta 152 aircraft. |
Fitted with the up-rated Jumo 213F series engine similar
to the Jumo 213E used in the Ta-152 H series but minus the intercooler.
Two 30 mm (1.18 in) MK 108 cannons were installed in the outer wings
to complement the 20 mm MG 151s in the inboard positions. |
Similar to the D-11,
but featured the 30 mm (1.18 in) MK 108 cannon in a Motorkanone
installation firing through the propeller hub. |
would be fitted with a 20 mm MG 151/20 motor cannon.
|
DIMENSIONS (Fw-190D-9 variant) |
3200 kg |
4300 kg |
4840 kg |
10.19 m |
10.51 m |
18.30 m² |
3.36 m |
233 kg/m² |
ARMAMENT (Fw-190D-9 variant) |
2 × 20 mm MG 151/20 E cannon
(1) |
2 x 250 |
2 × 13 mm (.51 in) MG 131 (2) |
2 x 475 |
1 × 250 kg bomb type SC-250,
centerline |
- |
(1) synchronized in the wing roots, (2)
synchronized in upper nose
POWERPLANT (Fw-190D-9 variant) |
1 ×
Junkers Jumo 213A-1 |
12-cylinder inverted
Vee, 35 L |
2100-2240
hp* |
488-520 hp / ton ** |
524
L plus provision for 115 L of auxiliary fuel in a rear-fuselage
tank (internal) + 1 x 300 L (80 US gal) drop tank
|
(*) with MW50 boost, (**) with loaded weight
PERFORMANCES (Fw-190D-9 variant) |
710 km/h
at 11000 m,
686 km/h at 6599 m |
575 km/h at sea level |
? km/h |
12000 m |
17 m/s |
835 km typical |
(*) vitesse de décrochage
|