After receiving mostly positive results with his F 19 and F
19a "Ente" (Duck) light transport aircraft, Focke proceeded
to design a twin-engined "Ente" (Duck) bomber for the fledgling
Luftwaffe in 1931. This aircraft went through several design changes (January
13, 1932 - December 25, 1933), mainly concerning the placement of the front
horizontal tail (canard) and the rear vertical tail. The first design placed
the forward canard above the fuselage, and there were two fins and rudders
mounted on the each wing end, with two more fins along the wing trailing
edge outboard of the engine nacelles. Windtunnel tests showed that directional
stability was only slightly better with the four fins than a large single
vertical fin and rudder. Therefore, the decision was made to go with the
single large fin, due to the lower component cost and ease of construction.
Also, the forward canard was moved down to the fuselage bottom, thus improving
the pilot's view and the forward gunner's field of fire. On all versions,
the fuselage was narrow and long, with open MG firing stations in the extreme
nose and tail. Two BMW VIu 12 cylinder engines (750 horsepower for takeoff)
were mounted beneath each wing, and were provided with a four bladed propeller
of 3.8 m (12' 6") in diameter. The landing gear was retractable and the
cockpit was located approximately mid-fuselage, with the forward fuselage
stepped down in front of the cockpit. A crew of 6 was to man the Fw 42.
A full sized
mock-up was built for the Fw 42, which was equipped with MG stations and
control units. It was visited by the Russians and/or Japanese, for possible
export license or production purchases. Although good results were reported
from the windtunnel tests, a construction contract was not issued, so all
work ceased on the Fw 42, which would have certainly been one of the most
unusual bombers ever constructed.
As a historical
note, almost the entire story of the Fw 42 would have been unknown except
for a series of fortuitous events. In 1945, the Fw 42 file was forgotten
in the evacuation of a shelter where Focke-Wulf had stored many of their
documents. Moments later, this shelter was blown up in an attempt to hide
any other data which could not be carried away. When the ruins of this
shelter were being cleared 24 years later, Georg Graf zu Dohna, arranged
with the excavators to pay attention in case anything of interest was uncovered.
Incredibly enough, a file was soon uncovered which contained all the Fw
42 data, including photos and 12 windtunnel reports, and were almost completely
undamaged, even though they had lain under the rubble for several
decades!
Span
(main wing) |
Span
(canard) |
Length | Height
(overall) |
Height @
forward fuselage |
Height @
cockpit |
Wing Area
(main wing) |
Wing Area
(canard) |
25 m
82' |
9.25 m / 10.1 m
30' 4" / 33' 2" |
17.7 m
58' 1" |
4.3 m
14' 1" |
1.65 m
5' 5" |
2.35 m
7' 9" |
108 m²
1162.5 ft² |
15.1 m² / 17.3 m²
162.5 ft² / 186.2 ft² |
Empty | Equipped | Takeoff | Bomb Load |
5600 kg
12346 lbs |
6500 kg
14330 lbs |
8500-9000 kg
18739-19842 lbs |
1000 kg
2205 lbs |
Max. Speed | Cruising Speed | Landing Speed | Ceiling | Range |
300-310 km/h
186-193 mph |
260 km/h
162 mph |
85 km/h
53 mph |
5000-6000 m
16404'-19685' |
1200-1800 km
746-1118 miles |
There are no scale models of the Fw 42 |
The first design of the Focke-Wulf Fw 42,
with the forward horizontal tail above the fuselage and four small rudders
attached on the rear wing. Factory photo number 666
Another view of the original
configuration of the Focke-Wulf Fw 42. Factory photo number 667
An amended wind tunnel model of the Fw 42, showing the forward canard
has now been moved beneath the fuselage, although the four vertical fins
remain at this time. Factory photo number 670
The final version of the Fw 42, now showing
the large, single vertical fin and ruddwr. Factory photo number 669
Another view of the final windtunnel model
of theFocke-Wulf Fw 42, the very narrow fuselage nose can be seen clearly
here. Factory photo number 668