Focke-Wulf Fw-190G
GENERAL DATA |
Würger |
Fighter
Close Support Attack Fighter
Fighter-bomber
Long range (attack) Fighter
|
1 |
Arado, Fieseler,
Focke-Wulf |
800 |
1941 |
1942 |
Variants |
was renamed from A-4/U8 JaBo Rei's. Initial testing
found that if all but two wing root mounted 20 mm MG 151 cannons (with
reduced ammunition load) were removed, the Fw 190 G-1 (as it was now
called) could carry a 250 kg or 500 kg bomb on the centreline and
up to a 250 kg bomb under each wing. |
was renamed from Fw 190 A-5/U8 aircraft, similar to
the G-1; the underwing drop tank racks were replaced with the much
simpler V.Mtt-Schloß fittings, to allow for a number of underwing
configurations. |
was based on A-6 with all but the two wing root mounted
MG 151 cannons removed. The new V.Fw. Trg bombracks, however, allowed
the G-3 to simultaneously carry fuel tanks and bomb loads |
The G-3/R1 replaced the V.Fw. Trg racks with Waffen-Behälter
WB 151/20 cannon pods, giving the G-3/R1 a total of six 20 mm cannon. |
was similar to the R1, but the V.Fw. Trg racks were
removed, and two ETC 50 racks per wing were added. |
was based on the Fw 190 A-8, using the same "bubble"
canopy as the F-8 and fitted with underwing ETC 503 racks that could
carry either bombs or drop tanks. |
was a planned refit for
the GM 1 engine boost system, but never made it into production. |
G-8/R5 kit replaced the ETC 503 racks with two ETC 50
or 71 racks. |
DIMENSIONS (Fw-190F-8 variant) |
3610 kg |
4400 kg |
5010 kg |
8.95 m |
10.51 m |
18.30 m² |
3.95 m |
241 kg/m² |
ARMAMENT (Fw-190F-8
variant) |
2 × 20 mm MG 151/20 E cannon
(1) |
2 x 250 |
- |
- |
Up to 1800 kg on three hardpoints:
center fuselage rated at 1800 kg, carrying 1 × 1800 kg
(SC-1800) bomb or 1 × 500 kg (SC-500) bomb
2 underwing units rated at 250 kg, carrying 2 × 551 lb (SC-250)
bombs, or 4 × 50 kg (SC-50) bombs
|
- |
(1) synchronized in the wing roots
POWERPLANT (Fw-190F-8
variant) |
1 ×
BMW 801 D-2 |
air-cooled 14-cylinder-radial,
41.8 L |
1700-2100
hp * |
339-419 hp / ton ** |
524
L plus provision for 115 L of auxiliary fuel in a rear-fuselage
tank (internal)
+ 900 L total, consisting of 3 × 300 L droptanks (external)
|
(*) with MW50 boost, (**) with max takeoffweight
PERFORMANCES (Fw-190F-8 variant) |
624 km/h
at 5000 m |
422 km/h at optimum altitude |
? km/h |
10601 m |
15 m/s |
641 km typical, 1049 km max |
(*) vitesse de décrochage
|