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Reichskriegsflagge |
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Third
Reich |
| Bomber Aircraft |
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German World War II
Bomber Aircraft |
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Dornier Do-215 |
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The Dornier Do 215 was a light bomber,
reconnaissance aircraft and later a night
fighter aircraft produced by Dornier Werke GmbH
originally produced for export, but in the event
all except two served in the Luftwaffe. It was
nicknamed "The Flying Pencil" because of its
slim fuselage. The successor of the Do 215 was
the Dornier Do 217.
The Dornier Do 17 fast bomber elicited renewed
interest from foreign air forces (after the
initial Do 17K series production). In July 1937,
Dornier therefore prepared a pre-series Do 17
Z-0 as a demonstrator for export customers. It
was given the civil registration D-AAIV. While
this aircraft was essentially identical to the
production Do 17Z, the
Reichsluftfahrtministerium assigned the
designation Do 215 to the export version.
The V1 prototype retained the 9-cylinder Bramo
323 Fafnir radial of the Do 17Z.
The second prototype (Do 215 V2) was equipped
with Gnome-Rhône 14-NO radial engines. It safely
completed testing, but did not attract export
orders because it did not offer a notable
performance increase over the Do 17Z. Dornier
therefore equipped the V3 prototype with the
1,175 PS (1,159 hp) Daimler-Benz DB 601Ba inline
engines (note: it is not the first time DB
engines where used in a Do 17 series). The V3,
which first flew in the spring of 1939, showed a
noticeable improvement in flight performance
compared to the earlier prototypes.
Series production of the Do 215 A-1 began
in 1939. The order, intended for the Swedish Air
Force, was stopped in August 1939 due to the
political situation. The 18 extant aircraft were
embargoed and pressed into Luftwaffe service
upon the outbreak of World War II.
Some modifications were made and the resulting
aircraft were redesignated Do 215B. This
was the standard production version. Between 92
and 105 (depending on sources) were produced
between 1939 and 1941.
The Luftwaffe initially operated the Do 215 as a
bomber and reconnaissance aircraft. Aircraft
equipped with the Rb 20/30 and Rb 50/30 cameras
were used for long-range reconnaissance
missions, primarily at the Ob.d.L (Oberkommando
der Luftwaffe). Later aircraft operated as night
fighters. The last of the Do 215s were retired
in late 1944.
General characteristics
-
Crew:
4 (pilot, bomb aimer/gunner, two gunners)
-
Length:
15.79 m (51 ft 9⅔
in)
-
Wingspan:
18 m (59 ft 0⅔
in)
-
Height:
4.56 m (14 ft 11½ in)
-
Wing area:
55 m² (592 ft²)
-
Empty weight:
5,780 kg (12,727 lb)
-
Loaded weight:
8,800 kg (19,404 lb)
-
Powerplant:
2× Daimler-Benz DB 601 Ba
V-12-cylinder
inline engines, 1,175 PS (1,159 hp, 864 kW)
each
Performance
-
Maximum speed:
470 km/h (254 knots, 292 mph) at 4000 m
(13,124 ft)
-
Range:
2,450km (1,323 nm, 1,522 mi) normal
-
Service ceiling
9,000 m (29,500 ft)
-
Wing loading:
105.1 kg/m² (32.78 lb/ft²)
-
Power/mass:
184 W/kg (0.113 hp/lb)
Armament
-
Four 7.92 mm MG 15
machine guns, later
upgraded to 6
-
1000 kg (2,200 lb) bombs
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Dornier Do-217 |
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The Dornier Do 217 was a
bomber used by Germany during
World War II. It was designed
from scratch as a replacement
for the earlier Dornier Do 17.
At the beginning of 1938,
Dornier issued manufacturing
specification No. 1323,
recognising the need for a twin
engined bomber or long range
reconnaissance aircraft powered
by Daimler-Benz DB 601B engines.
Dornier recognized shortcomings
of its fast Dornier Do 17 well
before the war. With Junkers'
new prototype, the Junkers Ju 88
being superior to the Do 17 in
every way, Dornier designed a
new bomber to meet a requirement
from the RLM for a larger and
more versatile bomber than the
Do 17, capable of both level and
dive bombing. One of the most
versatile and useful bomber
designs the Germans put into
production after the war
started, the Dornier Do 217
remedied the shortcomings of the
Do 17 while greatly advancing
the design in all areas.
Superficially a scaled up
Dornier Do 215, and initially
powered by the same engines, the
Do 217 was actually considerably
larger and totally different in
detailed design. The first
prototype (the Do 217 V1)
flew on 4 October 1938, but
crashed seven days later during
a single engine flying test.[1]
It was found to be underpowered
and was unmanoeuvrable when
compared with contemporary
bombers. Instability was a
problem at first, but
modifications such as fixed
slats along the leading edges of
the vertical fins helped to
improve flight stability.
Much of Dornier's efforts in
1938 to 1940 were devoted to
finding more powerful engines
and improving the flying
qualities. When the BMW 801
radial engine became available,
it solved the problems of the
aircraft being underpowered and
allowed the fuselage to be
deepened, thus accommodating
larger and heavier bomb loads.
This enabled the Do 217 to
fulfil its potential and carry a
heavier bomb load than any other
Luftwaffe bomber of the time.
There was a desire for the Do
217 to be capable of performing
dive bomber duty, so it was
therefore fitted with a tail
mounted air brake. This could
not be made to function
adequately in the early models
however, and was omitted until
the Do 217E-2 entered service.
When this mark reached service,
use of the dive brake was found
to sometimes overstrain the rear
fuselage, so the dive brakes
were often removed.
In almost every way, the Do 217
was a success. It could carry a
much heavier bombload than
either the Heinkel He 111 or the
Junkers Ju 88. It was also very
fast, surpassing both aircraft
in maximum speed. It was
Germany's largest bomber for
nearly two years until the
Heinkel He 177 was finally safe
enough to use. Do 217s sank the
Italian battleship Roma
with Fritz X missiles as she
steamed to the Allies after
Italy's capitulation. Do 217s
were phased out of combat use in
mid 1944.
Like the Do 17 and the Ju 88,
the aircraft was used in a
variety of roles, including that
of the night-fighter - a sign
that Germany desperately needed
fighters far more than it needed
bombers. Production was stopped
in April 1944 in favor of
single-engined fighters.
Operational use of the Do 217 as
a night-fighter was restricted
in 1943 to NJG 4. The only
capability in which the Do 217
was used up to the end of the
war was as a night
reconnaissance plane. Like the
Do 17, this important type of
service in the Luftwaffe is
frequently overlooked.
The Do 217 was built in series
from November 1940 to May 1944.
In 1943, 395 aircraft could not
be delivered to the Luftwaffe
due to shortages of the DB 603
engines used in the M-1 and N-1
versions. These aircraft were
stored, and while some were
refitted in 1944 when the
engines became available, the
remainder (around 125) were
scrapped. The Do 217 was only
built by the three Dornier
companies: Dornier
Friedrichshafen (DWF): 316
aircraft, Dornier München (DWM):
985 aircraft and Norddeutsche
Dornier-Werke (NDW): 602
aircraft. Production stopped in
Friedrichshafen in December
1942, and in Wismar (NDW) in
October 1943.
General characteristics
-
Crew:
3
-
Length:
18.20 m (59 ft 8½ in)
-
Wingspan:
19.00 m (62 ft 4 in)
-
Height:
5.00 m (16 ft 5 in)
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Wing area:
57.00 m² (613.54 ft²)
-
Empty weight:
9,350 kg (20,615 lb)
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Max takeoff weight:
13,180 kg (29,059 lb)
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Powerplant:
2× BMW 801A
14-cylinder
radial engine, 1,560 PS
(1,539 hp, 1,147 kW) each
Performance
-
Maximum speed:
487 km/h at 5,500 m (303 mph
at 18,045 ft)
-
Range:
2,050 km (1,274 miles)
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Service ceiling
8,400 m (27,560 ft)
Armament
-
4 x 7.92 mm MG 17
machine
guns in nose with 1,000 rpg
-
4 x 20 mm MG FF
cannons in
nose with 250 rpg
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2 x 13 mm MG 131
machine
guns in dorsal and ventral
positions with about 500 rpg
apiece
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Heinkel He-111 |
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The Heinkel He 111 was a
German medium bomber designed by
Siegfried and Walter Günter in
the early 1930s in violation of
the Treaty of Versailles. The
Heinkel became the most numerous
and primary Luftwaffe bomber
during the early stages of World
War II. It is perhaps the most
famous symbol of the German
bomber force (Kampfwaffe)
due its distinctive "Greenhouse"
nose.
The He 111 took on the mantle of
"workhorse", and was used in a
variety of roles on every front
in the European Theatre
throughout the war. It was used
as a strategic bomber during the
Battle of Britain, a torpedo
bomber during the Battle of the
Atlantic, a medium bomber and a
transport aircraft on the
Western Front, Eastern Front and
Mediterranean and North African
Fronts. It became obsolete, but
the failure to design and
produce a successor meant the He
111 continued to be produced
until 1944, when piston-engined
bomber production was largely
halted, in favour of fighter
aircraft.
The design of the Heinkel
endured after the war in the
CASA 2.111. Its airframe was
produced in Spain under license
by Construcciones Aeronáuticas
SA. The design differed
significantly in powerplant
only. The Heinkel's descendant
continued in service until 1973,
when it was retired.
In the early 1930s, Ernst
Heinkel decided to build the
world's fastest passenger plane,
a lofty goal met by more than a
little skepticism by the German
aircraft industry and its newly
evolving political leadership.
Heinkel entrusted the
development to Siegfried and
Walter Günter, fairly new to the
company and untested.
The aircraft was superior to the
already fast Lockheed 9 Orion
that their design was competing
against. The first example of
their soon-to-be-famous Heinkel
He 70 Blitz (“Lightning”)
rolled off the line in 1932 and
immediately started breaking
records. In its normal
four-passenger version, its
speed almost reach 200 mph (320
km/h), even though it was
powered by only a single 600 hp
(447 kW) BMW V1 engine. The
elliptical wing, which the
Günther brothers had already
used in the Bäumer Sausewind
sports plane before they joined
Heinkel, became a feature in
many subsequent designs the
brothers developed. The design
immediately garnered the
interest of the Luftwaffe, which
was looking for medium bombers
for military service.
The future Heinkel He 111 was a
more powerful twin-engine
version of the Blitz,
producing an aircraft that had
many of the Blitz's
features, including its
elliptical inverted gull wing,
small rounded control surfaces,
and BMW engines. With location
of the engines the only notable
change in appearance, the new He
111 design was often called the
Doppel-Blitz (“Double
Lightning”).
At 14,000 kg take-off weight
(carrying 2,000 kg of bombs
internally), the He 111H
achieved a top speed of 405 km/h
at 6 km, improving to 435 km/h
without the bomb load and at 50%
fuel load. Still, this was
considerably slower than the
newer Junkers Ju 88 which
entered service in 1940, so the
He 111 was gradually withdrawn
from the bomber role. The He 111
became a jack-of-all-trades as
the war progressed, carrying out
missions not even imagined when
the war started.
Nevertheless, the He 111 had to
be kept in production until 1944
because the RLM failed to
provide a successor: the He 177
Greif heavy bomber was
plagued by engine problems, and
the Bomber B program was
eventually abandoned. The vast
majority of the 7,300 He 111s
produced would be the H models,
largely identical to the first H
introduced in 1939.
General characteristics
-
Crew:
5 (pilot,
navigator/bombardier, nose
gunner, ventral gunner,
dorsal gunner)
-
Length:
16.4 m (54 ft 6 in)
-
Wingspan:
22.5 m (74 ft 3 in)
-
Height:
3.9 m (13 ft 9 in)
-
Wing area:
86.5 m² (942 ft²)
-
Empty weight:
7,720 kg (17,000 lb)
-
Loaded weight:
12,030 kg (26,500 lb)
-
Max takeoff weight:
14,075 kg (31,000 lb)
-
Powerplant:
2× Jumo 211F-1
liquid-cooled
inverted V-12, 986 kW (1,300
hp) each
Performance
-
Maximum speed:
400 km/h (250 mph)
-
Range:
2,800 km with max fuel
(1,750 mi)
-
Service ceiling
8,390 m (27,500 ft)
-
Rate of climb:
20 minutes to 5,185 m
(17,000 ft)
-
Wing loading:
137 kg/m² (28.1 lb/ft²)
-
Power/mass:
.082 kW/kg (.049 hp/lb)
Armament
-
Guns:
-
up to seven 7.92 mm MG
15
or MG 81 machine
guns, some of them
replaced or augmented by
-
1× 20 mm MG FF
cannon (central nose
mount or forward
ventral position)
-
1× 13 mm MG 131
machine gun (mounted
dorsal and/or
ventral rear
positions)
-
Bombs:
-
up to 2,000 kg (4,409
lb) carried internally
(eight 250 kg max),
or:
-
up to 2,500 kg (5,512
lb) on two external
racks
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Heinkel He-177 (Greif) |
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The Heinkel He 177 Greif
(Griffin) was a long-range
bomber of the Luftwaffe. The
troubled aircraft was the only
heavy bomber built in large
numbers by Germany during World
War II. Aircrews nicknamed it
the Luftwaffenfeuerzeug
(Luftwaffe's lighter) or the
'Flaming Coffin' due to the
engines' tendency to catch fire
on the early versions of the
aircraft.
Earlier versions had many
problems; when the problems were
solved the type was successful,
but could not be deployed in
quantity due to Germany's
deteriorating situation in the
war.
The He 177 was conceived as a
result of an
Reichsluftfahrtministerium (RLM)
requirement called the Bomber
A specification which called
for a bomber aircraft more
advanced than the Dornier Do 19
or Junkers Ju 89 Ural-Bomber
prototypes, capable of carrying
a bombload of at least 1,000 kg
(2,204 lb) over a range of 6,695
km (4,160 miles). The aircraft
had to possess a maximum speed
of about 540 km/h (335 mph) at
altitude and it had to embody
sufficient structural strength
to enable it to undertake medium
degree (later changed to 60
degree) diving attacks. In order
to meet these specifications the
He 177 embodied many advanced
features including coupled
engines with surface evaporation
cooling and small remotely
controlled defensive gun
turrets.
An unusual feature of the
aircraft was the use of twin
engines in each nacelle driving
a single propeller, as the
components of a "power system".
Siegfried Günther, chief
designer of Heinkel, chose to
use the Daimler-Benz DB 606,
which consisted of two
Daimler-Benz DB 601 engines
coupled together to use a common
propeller, in order to minimise
drag. The two engines were
coupled side by side in each
nacelle and inclined inwards at
the crankcases' upper surfaces,
so that the inner cylinder banks
were disposed almost vertically,
a single gear casing connecting
the two crankcases, and the two
crankshaft pinions driving a
single airscrew shaft gear. The
insistence of this engine
configuration stemmed directly
from the RLM's determination
that the He 177 should be
capable of dive bombing. The use
of only two propellers on a
heavy bomber also offered a
substantial reduction in drag
and a marked improvement in
maneuverability. Indeed, the
initial prototypes and
pre-production models of the
bomber had an airspeed and
maneuverability comparable to
many heavy fighters of the time.
Both the DB 606 and 610 coupled
"power systems" had A and B
versions, signifying opposing
rotation directions when in
operation-the He 177 V1 through
V3 prototypes all had the A-1
version, that rotated
counterclockwise when seen from
the front, used on both sides,
while all later 177s, from the
V4 prototype onwards through the
entire production run, used one
A- and one B-version of the
engines, using one of the
clockwise-rotation B-versions on
the port-side wing.
Beset by many other technical
difficulties in development and
service, the plane had a
troubled life. This was in part
due to overly optimistic design
requirements of long range, high
speed, heavy bomb load, and dive
bombing. Though Goering forbade
Heinkel to develop a version
with four separate nacelles,
Heinkel nevertheless produced
prototypes of the Heinkel He
177B (later renamed Heinkel He
277) which was produced in
limited numbers.
Although the He 177 entered
service in 1942 it was still far
from operational. As an
emergency measure it was used to
supply the encircled 6th Armee
at Stalingrad where it was
determined that it could only
carry about the same cargo
payload as the appreciably
smaller Heinkel He 111, and was
useless for the evacuation of
wounded troops. As a result the
He 177s reverted to bombing and
flak-suppression missions in
support of the Wehrmacht in the
vicinity of Stalingrad. Only
thirteen missions were flown and
seven of the He 177's crashed in
flames without any action
attributable to the enemy.
General characteristics
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Crew:
5
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Length:
22 m (72 ft 2 in)
-
Wingspan:
31.44 m (103 ft 1 in)
-
Height:
6.7 m (21 ft)
-
Wing area:
101.5 m² (1,092 ft²)
-
Empty weight:
16,800 kg (37,000 lb)
-
Loaded weight:
31,000 kg (68,340 lb)
-
Powerplant:
2× Daimler-Benz DB 610
(twin
DB 605) 24-cylinder
liquid-cooled inline
engines, 2,950 hp (2,170 kW)
each
Performance
-
Maximum speed:
565 km/h (350 mph) at 6,100
m (21,000 ft)
-
Combat radius:
1.540 km (960 mi)
-
Ferry range:
5,600 km (3,200 mi)
-
Service ceiling
9,400 m (30,800 ft)
-
Wing loading:
319.9 kg/m² (65.6 lb/ft²)
-
Power/mass:
110 W/kg (0.067 hp/lb)
Armament
-
Guns:
-
2 x 20 mm MG 151
cannon
-
3 x MG 131
machine gun
-
3 x MG 81
7.92mm
machine gun
-
Bombs:
up to 7,200 kg (15,873 lb)
of bombs or 3 guided
missiles (Henschel Hs 293 or
Fritz X)
Usual configuration:
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48 x 70 kg bombs (3,360
kg/7,405 lb total)
-
10 x 500 kg bombs (5,000
kg/11,020 lb total)
-
6 x 1000 kg bombs (6,000
kg/11,224 lb total)
-
2 x 2500 kg bombs (5,000 kg/
11,020 lb total)
or
-
2 Hs 293 + 1 Hs293 remotely
controlled missiles under
the fuselage
-
2 Hs 294 + 1 Hs 294 remotely
controlled glide bombs under
the fuselage
-
2 PC 1400 + 1 PC 1400
gliding bomb under the
fuselage
-
2 torpedoes + 2 torpedoes
under the fuselage
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Junkers Ju-86 |
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The Junkers Ju 86 was a German monoplane
bomber
and civilian
airliner designed in the early 1930s by
Junkers.
The civilian model Ju 86B could carry ten
passengers; two were delivered to
Swissair and five to
Lufthansa. It was used by both sides in
World War II. Furthermore a single civilian Ju 86Z was delivered to the Swedish
AB Aerotransport.
The bomber was
field tested in the
Spanish Civil War,
where it proved inferior to the
Heinkel He 111.
Four Ju 86D-1 arrived in Spain in early February
1937, but after a few sorties one of them (coded
26-1) was shot down on 23 February by Republican
fighters with the loss of 3 crewmen killed and 1
captured. A replacement plane was sent from
Germany, but in the summer of 1937 another D-1
was lost in an accident, and the three remaining
planes were sold to the Nationalist air forces.
It was again used in the 1939 invasion of
Poland, but retired soon after. In January 1940
the
Luftwaffe
tested the prototype Ju 86P with a longer
wing span,
pressurized cabin,
Jumo 207A1 turbocharged
diesel engines, and a two-man crew. The Ju 86P
could fly at heights of 12,000 m (39,000 ft) and
higher on occasion, where it was felt to be safe
from Allied fighters. The
Westland Welkin
and
Yakovlev Yak-9PD were developed specifically to counter this threat.
No. 12 Squadron SAAF used Ju 86 bombers in the
East African Campaign.
Satisfied with the newer version, the Luftwaffe
ordered that some 40 older-model bombers be
converted to Ju 86P-1 high altitude
bombers and Ju 86P-2 photo reconnaissance
aircraft. Those operated successfully for some
years over Britain, the Soviet Union and North
Africa. In August 1942, a modified
Spitfire V
shot one down over Egypt at some 49,000 ft
(14,500 m); when two more were lost, Ju 86Ps
were withdrawn from service in 1943.
Junkers developed the Ju 86R for the
Luftwaffe, using larger wings and new engines
capable of even higher altitudes — up to 16,000
m (52,500 ft) — but production was limited to
prototypes.
General characteristics
-
Crew:
2 (pilot and radio operator)
-
Length:
16.46 m (54 ft)
-
Wingspan:
32 m (105 ft)
-
Height:
4.7 m (15 ft 5 in)
-
Wing area:
82 m² (883 ft²)
-
Empty weight:
6,700 kg (14,800 lb)
-
Max takeoff weight:
11,530 kg (25,420 lb)
-
Powerplant:
2×
Junkers Jumo 207B-3/V,
2-stroke,
6cyl, 12 piston,
diesel engines,
746 kW (1,000 hp) each
Performance
-
Maximum speed:
420 km/h (260 mph) above 9,150 m (30,000 ft)
-
Range:
1,580 km (980 mi)
-
Service ceiling
13,000 m (42,650 ft)
-
Rate of climb:
4.67 m/s (900 ft/min)
-
Wing loading:
kg/m² (lb/ft²)
-
Power/mass:
W/kg (hp/lb
Armament
-
Guns:
-
3 x
MG15
machine guns
|

Junkers Ju-87 (Stuka) |
|
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The Junkers Ju 87 or Stuka (from
Sturzkampfflugzeug,
"dive
bomber") was a two-seat (pilot and
rear gunner)
German
ground-attack aircraft
of
World War II. Designed by Hermann Pohlmann, the Stuka first flew in 1935 and
made its combat début in 1936 as part of the
Luftwaffe's
Condor Legion during the
Spanish Civil War.
The aircraft was easily recognizable by its
inverted
gull wings,
fixed
spatted undercarriage and its infamous Jericho-Trompete
("Jericho Trumpet") wailing
siren,
becoming the
propaganda symbol of German
air power and the
Blitzkrieg
victories of 1939-1942. The Stuka's design
included several innovative features, including
automatic pull-up
dive brakes under both wings to ensure that the plane
recovered from its attack dive even if the pilot
blacked out
from the high acceleration. Although sturdy,
accurate, and very effective, the Ju 87 was
vulnerable to modern fighter aircraft, like many
other
dive-bombers of the war. Its flaws became apparent during the
Battle of Britain - poor manoeuvrability, lack of speed and defensive
armament meant that the Stuka required a
fighter escort to operate effectively.
The Stuka operated with further success
after the Battle of Britain, and its potency as
a precision ground attack aircraft became
valuable to the German war effort in the
Balkans Campaign, the
African and Mediterranean Theatres and the early stages of the
Eastern Front
campaigns where Allied fighter resistance was
disorganised and in short supply. However, once
the Luftwaffe had lost
air superiority on all fronts the Ju 87 once again
became easy targets for enemy fighter aircraft.
In spite of this, and lacking a successor, the
type continued to be produced until 1944. By the
end of the conflict the Stuka was largely
replaced by ground attack versions of the
Focke-Wulf Fw 190, but some units, like
Sturzkampfgeschwader 2
"Immelmann" operated the Ju 87 to the last day of the war. 5,752 Ju 87 of all
versions were built between 1936 and August
1944.
Hans-Ulrich Rudel was the most notable Stuka
ace
and was the most highly decorated German
serviceman of World War II.
The Ju 87's principal designer, Hermann Pohlmann,
held the opinion that any dive-bomber design
needed to be simple and robust. This led to many
technical innovations, like retractable
undercarriage, being removed from the design,
and also led to one of the Stuka's
distinctive features, its fixed and "spatted"
undercarriage. Pohlmann continued to carry on
developing and adding to his and Karl Plauth's
ideas (Plauth was killed in a flying accident in
November 1927), and produced the Ju A 48 which
underwent testing on
29 September
1928.[1] The military version
(designation) of the Ju A 48 was the Ju K 47.
In the early 1920s the Dessau-based Junkers
Flugzeugwerke AG had concentrated
upon military rather than civil aircraft,
although these machines as yet had "uncranked"
wings and twin tail-fin units. Because of the
Versailles Treaty of 1919, which stated that Germany was not permitted to
produce warplanes, the Ju K 48 was assembled and
rebuilt to K 47 outside Germany by Junkers-owned
subsidiaries, such as AB Flygindustri in Malmö,
Sweden.
After the Nazis came to power the design was
given priority. Despite initial competition from
the
Henschel Hs 123 the Reichsluftfahrtministerium (RLM: "Aviation
Ministry"), turned to the designs of Herman
Pohlmann of Junkers and co-designer of the K 47,
Kark Plauth.
During the trials with the K 47 in 1932, the
double
vertical stabilizers
were introduced to give the rear gunner a better
field of fire.
The main, and what was to be the most
distinctive feature of the Ju 87, was its
double-spar inverted
gull wings.
Diving procedure
Flying at 4,600 meters (15,000 ft), the pilot
located his target through a bombsight window in
the cockpit floor. After opening the dive
brakes, retarding his throttle, and closing the
coolant flaps, he then rolled the aircraft 180°,
automatically nosing the aircraft into a dive.
Red tabs protruded from the upper surfaces of
the wing as a visual indicator to the pilot that
in case of a
g induced black-out, the automatic dive recovery system would be
activated. The Stuka dived at a 60 - 90 degree
angle, accelerating to 600 km/h (350 mph).
When the aircraft was reasonably close to the
target, a light on the contact
altimeter came on to indicate the bomb-release point, usually at a minimum
height of 450 m (1,500 ft). The pilot released
the bomb by depressing a knob on the control
column to release weapons and to initiate the
automatic pull-out mechanism. An elongated
U-shaped crutch located under the fuselage would
swing the bomb out of the way of the propeller,
and the aircraft would automatically begin a 6
g pullout.
Once the nose was above the horizon, dive brakes
were retracted, the throttle was opened, and the
propeller was set to climb. The pilot regained
control and resumed normal flight. The coolant
flaps had to be reopened quickly.
In his book Wings of the Luftwaffe, Royal
Navy test pilot
Eric "Winkle" Brown reported that a captured Ju 87 D-3 he test-flew after the war felt
"absolutely right" diving at a 90° straight down
angle, and stated that he had no doubt of the
Stuka's ability in its assigned role.
General characteristics
-
Crew:
2
-
Length:
11.00 m (36 ft 1.07 in)
-
Wingspan:
13.8 m (45 ft 3.30 in)
-
Height:
4.23 m (13 ft 10.53 in)
-
Wing area:
31.90 m² (343 ft² 53.09 in²)
-
Empty weight:
3,205 kg (7,086 lb)
-
Loaded weight:
4,320 kg (9,524 lb)
-
Max takeoff weight:
5,000 kg (11,023 lb)
-
Powerplant:
1×
Junkers Jumo 211D
liquid-cooled inverted-vee
V12 engine, 1200 PS (1184 hp, 883 kW)
-
Propellers:
Three-bladed Junkers VS 5 propeller, 1 per
engine
-
Propeller diameter:
3.4 m (11 ft 1.85 in)
Performance
-
Never exceed speed:
600 km/h (373 mph)
-
Maximum speed:
242 mph @ 13,410 ft or (390 km/h @ 4,400 m)
-
Range:
500 km (311 mi) with 500 kg (1,102 lb) bomb
load
-
Service ceiling
8,200 m (26,903 ft) with 500 kg (1,102 lb)
bomb load
Armament
-
Guns:
2× 7.92 mm MG 17
forward, 1× 7.92 mm MG 15
to rear
-
Bombs:
Normal load = 1× 250 kg (551 lb) bomb
beneath the fuselage and 2× 50 kg (110 lb)
bombs underneath each wing.
|

Junkers Ju-88 |
|
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The Junkers Ju 88 was a World War II Luftwaffe
twin-engine, multi-role aircraft. Designed by Hugo Junkers in
the mid 1930s, it became one of the most versatile combat
aircraft of the war. The Ju 88 suffered from a number of
technical problems during the later stages of its development
and early operational roles. Like a number of other Luftwaffe
bombers, it was used successfully as a bomber, dive bomber,
night fighter, torpedo bomber, reconnaissance aircraft, heavy
fighter, and even as a flying warhead during the closing stages
of conflict. Despite its protracted development, the aircraft
became one of the Luftwaffe's most crucial assets. There were
15,000 Ju 88s built during World War II, more than any other
twin-engined German aircraft of the period.
In October 1937 Generalluftzeugmeister Ernst Udet had
ordered the development of the Ju 88 as a heavy dive-bomber.
This decision was influenced by the success of the Junkers Ju 87
Stuka in this role. The Junkers development center at
Dessau gave priority to the study of pull-out systems, and dive
brakes. The first prototype to be tested as a dive-bomber was
the Ju 88 V4 followed by the V5 and V6. These models became the
planned prototype for the A-1 series. The V5 made its maiden
flight on 13 April 1938, and the V6 on 28 June 1938. Both the V5
and V6 were fitted with four bladed propellers, an extra bomb
bay and a central "control system". As a dive bomber, the Ju 88
was capable of pinpoint deliveries of heavy loads; however,
despite all the modifications, dive bombing still proved too
stressful for the airframe, and in 1943, tactics were changed so
that bombs were delivered from a shallower, 45° diving angle.
Aircraft and bomb sights were accordingly modified and dive
brakes were removed. With an advanced Stuvi dive-bomb sight,
accuracy remained very good for its time. Maximum bomb load of
the A-4 was 2,500 kg, but in practice, standard bomb load was
1,500 to 2,000 kg. Junkers later used the A-4 airframe for the
A-17 torpedo carrier. However the variant lacked a ventral gun
position.
The standard fighter-bomber version became the Ju 88C-6,
applying experience acquired with the A-4 bomber, equipped with
the same Jumo 211J engines. The C-6 was used mostly as
fighter-bomber and therefore assigned to bomber units. As a
reaction to the increasing number of attacks on German shipping,
especially on U-boats in the Bay of Biscay, from July 1942
started flying anti-shipping patrols and escort missions from
bases in France.
The aircraft of V./KG 40 (which was redesignated I./Zerstörergeschwader
1
in 1943) were a significant threat to the antisubmarine aircraft
and operated as escort fighters for the more vulnerable
Focke-Wulf Fw 200
Condor bombers. Between July 1942 and July 1944, the Ju 88s of
Kju88and ZG 1 were credited with 109 confirmed air-to air
victories, at a cost of 117 losses. They were
finally deployed against the Allied
Invasion of Normandy
in June 1944, incurring heavy losses for little effect before
being disbanded on
5 August
1944.
General
characteristics
-
Crew:
4
-
Length:
14.36 m (47 ft 2⅞ in)
-
Wingspan:
20.08 m (65.88 ft)
-
Height:
5.07 m (16.63 ft)
-
Wing area:
54.7 m² (587 ft²)
-
Loaded
weight:
9,000 kg (20,000 lb)
-
Max
takeoff weight:
14,000 kg (30,865 lb)
-
Powerplant:
2×
Junkers
Jumo 211J
liquid-cooled inverted V-12, 1,044 kW (1,420 PS, 1,401 hp)
each
Performance
-
Maximum
speed:
475 km/h (295 m) at 5,300 m (17,388 ft)
-
Range:
2,300 km (max internal fuel) (1,429 mi)
-
Service
ceiling
8,500 m (26,900 ft)
Armament
-
Guns:
-
3-6
machine guns, either
MG
15
,
MG
81 ,
MG 81Z or
MG
131 ,
with one each firing forward from both main cockpit
windscreen glazing, and undernose Bola gondola,
and one or two guns firing from the rear of the main
cockpit (some carried one
MG
FF cannon
in the nose)
-
Bombs:
Max load 2,005kg (4,420 lb)
-
Ten
50kg (110 lb) bombs internally + four 250kg (551 lb)
bombs externally.
-
Two
500kg (1,105 lb) externally.
-
Four
500kg (1,105lb) bombs externally.
|
 Junkers Ju-188 (Reacher) |
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The Junkers Ju 188 Rächer (Reacher)
was a
German
World War II
high-performance
medium bomber from
Junkers, the planned follow-on to the famed
Ju 88 with better performance and payload. It was produced only in
limited numbers, due both to the presence of
improved versions of the Ju 88, as well as the
deteriorating war condition and the resulting
focus on fighter production.
The prototype Ju 88B V1, D-AUVS, flew for
the first time with the 801A/B engines in early
1940. The fuselage was identical to the Ju 88
A-1, which presented a problem: with the extra
power, 1,560 PS (1,539 hp, 1,147 kW), the design
could now carry considerably more load than the
small bomb bay could fit. An additional external
shackle was then added to each wing well outside
the engines, although using the rack would
seriously hamper performance.
By 1942 it was becoming clear that the Ju 288
wasn't going to be ready any time soon, and at
the same time the Ju 88's were increasingly at
the mercy of a rapidly improving RAF and
Soviet
VVS.
The RLM finally decided that even the small
gains in performance in the Ju 88B were worth
considering, and asked Junkers for a series of
upgrades as the Ju 188.
The sole Ju 88 E-0 was modified with several
additional guns, another MG 131 firing rearward
just below the turret, one firing forward
through the nose, and the twinned
MG 81Z in the ventral bulge firing rearward. Two other airframes had
their engines and outer wings removed to act as
testbeds for water ditching, as it was planned
to use the Ju 188 in long overwater flights
against British shipping. A second Ju 188 test
airframe was also built up from another Ju 88
A-4, this one including a larger, more
trapezoidal vertical tail surface set to provide
more directional control at higher altitudes, a
feature also used on future Ju 88 models, such
as the Ju 88G night fighters. Originally known
as Ju 88 V44, this airframe was later designated
Ju 188 V1.
October 1942 the program was given the go-ahead
to start planning for production. A second
prototype was delivered in January, which moved
the outer bomb shackles to a position inboard of
the engines. Both started testing the dive
bombing system installed in the 88 A-4 in
February. The RLM then asked for another change,
allowing the aircraft to mount either the BMW
801 or Jumo 213 engines as a complete "power
egg", or Kraftei, that would simply be
bolted on and hooked up. Concerns about the Jumo
213, now years overdue, were offset by this
engine's better altitude performance, so it made
sense to delay the aircraft slightly if that
meant it could switch to the 213 as soon as they
became available. The second Ju 188 V1
prototype was flown in 1943.
In 1943 it was planned to upgrade the entire
lineup with even more wing area and a
pressurized cockpit for high-altitude work. A
single basic airframe would be offered in three
versions, the Ju 188J
heavy fighter,
Ju 188K bomber, and the Ju 188L
reconnaissance version. All three did away with
the under-slung gunner's compartment, leading to
a cleaner nose profile, and the bomber and recce
versions mounted their loads in a long pannier
under the middle of the plane instead of the
deeper fuselage of the G and H models.
Simpler versions of these with no defensive
armament and even longer wings became the Ju
188S fighter and Ju 188T intruder.
With Jumo 213 E-1 engines 2,050 PS (2,022 hp,
1,508 kW) at take-off and 1,690 PS (1,667 hp,
1,243 kW) at 9,500 m (31,400 ft), the Ju 188T
could reach 700 km/h (435 mph). Operating at
this altitude, the Ju 188S could carry only 800
kg of bombs.
Before any of these could start production, the
entire lineup was renamed the
Ju 388, the vastly improved performance warranting this change in name.
General characteristics
-
Crew:
5
-
Length:
15 m (49 ft 1 in)
-
Wingspan:
22 m (72 ft 2 in)
-
Height:
4.4 m (14 ft 7 in)
-
Wing area:
56 m² (603 ft²)
-
Empty weight:
9,900 kg (21,825 lb)
-
Loaded weight:
14,500 kg (31,967 lb)
-
Powerplant:
2× 1
BMW 801 G-2
,
1,250 kW (1,700 PS) each
Performance
-
Maximum speed:
499 km/h (310 mph)
-
Range:
2,190 km combat (1,360 miles)
-
Service ceiling
9,500 m (31,170 ft)
-
Wing loading:
258.9 kg/m² (53.0 lb/ft²)
-
Power/mass:
0.175 kW/kg (0.106 hp/lb)
Armament
-
Guns:
-
1 × MG 151 20 mm
cannon
-
3 × MG 131 13 mm
machine gun
-
Bombs:
|
 Junkers Ju-390 |
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The Junkers Ju 390 was a long-range derivative of the
Junkers Ju 290, and was intended to be used as a heavy
transport, maritime reconnaissance aircraft, and long-range
bomber. It was one of the aircraft (along with the Messerschmitt
Me 264 and Focke-Wulf Ta 400) submitted for the abortive
Amerika Bomber project.
Two prototypes were created by attaching an extra pair of
inner-wing segments onto the wings of basic Ju 90 and Ju 290
airframes, and adding new sections to lengthen the fuselages.
The first prototype, the V1, (serial marking GH+UK), was
modified from a Ju 90 V6 airframe (werke number J4918, civil
registration D-AOKD from July 1940 to April 1941, then to the
Luftwaffe as KH+XC, from April 1941 through April 1942, then
returned to Junkerswerke and used for Ju 390 V1 construction).
It made its maiden flight on
October 20,
1943
and performed well, resulting in an order for 26 aircraft, to be
designated Ju 390 A-1. None of these were actually built
by the time that the project was cancelled (along with Ju 290
production) in mid-1944.
The second prototype, the V2 (RC+DA), was longer than the V2
because it was constructed from a Ju 290 airframe (using the
fuselage of Ju 290 A1 werke number J900155).
The maritime reconnaissance and long-range bomber versions were
to be designated the Ju 390 B and Ju 390 C,
respectively. It has been suggested that the bomber could have
carried the
Messerschmitt Me 328
parasite fighter for self-defense, and some test flights are believed to
have been performed by a Ju 390 prototype equipped with the
anti-shipping
Fritz X guided
glide bomb.[
The V1 was constructed and largely assembled at Junkers' plant
at
Dessau,
Germany, and the first test flight took place on
October 20
1943. It's performance was satisfactory enough that the Air
Ministry ordered 26 in addition to the two prototypes. However,
the contracts for the 26 Ju 390s were cancelled in June 1944 and
all work ceased in September of that year.
On
November 26, 1943, the Ju 390 V1, with many other new aircraft and prototypes,
was shown to Adolf Hitler at
Insterburg,
East Prussia.
According to former Junkers
test pilot
Hans-Joachim Pancherz'
logbook, the Ju 390 V1 was brought to Prague immediately after
it had been displayed at Insterburg, and while there took part
in a number of test flights, which continued until March 1944,
including tests of
inflight refueling.[4]
The Ju 390 V1 was returned to Dessau in November 1944, where it
was stripped of parts and finally destroyed in late April 1945
as the American Army approached.
V2
The Ju 390 V2 was assembled in Bernburg, was first flown in
October 1943, and is said to have been configured for the
maritime reconnaissance role. Its fuselage had been extended by
8.2 feet (2.5 m), and it was equipped with FuG 200 Hohentwiel
ASV (Air to Surface Vessel) radar and defensive armament
consisting of 5x 20mm cannons. Green notes different armament,
specifically 4x 20mm cannon and 3x MG131 machine guns.
Test pilot Oberleutnant Eisermann recorded in his logbook that he flew
the V2 prototype (RC+DA) as late as February 1944. However,
Kössler and Ott state that the Ju 390 V2 was only completed
during June 1944, with flight tests beginning at the end of
September 1944.
A
Ju 390 which may or may not have been the V2 is claimed by some
to have made a test flight from Germany to
Cape Town
in early 1944. The sole source for the story is a speculative
article which appeared in the
Daily Telegraph in 1969 titled Lone Bomber Raid on New York Planned by
Hitler, in which Hans Pancherz reportedly claimed to have
made the flight in question. Author James P. Duffy has carried
out extensive research into this claim, which has proved
fruitless. Kössler and Ott make no mention of this claim either,
despite having themselves interviewed Pancherz.
New York flight
The first public mention of the alleged flight of a Ju 390 to
North America appeared in the
November 11 1955 issue of the British magazine RAF
Flying Review, of which aviation writer
William Green
was an editor. The magazine's editors were sceptical of the
claim, which asserted that two Ju 390s had made the flight, and
in March 1956 they published a letter from a reader which
claimed to clarify the account. This letter stated that a single
aircraft had made the flight and that it had reached a point
about 12 miles (19 km) miles off the US east coast, just north
of NYC.
According to Green , in June 1944 Allied Intelligence had learnt
from prisoner interrogations that a Ju 390 had been delivered in
January 1944 to FAGr 5 (Fernaufklärungsgruppe 5), based at
Mont-de-Marsan near
Bordeaux, and that it had completed a 32-hour
reconnaissance flight to within 12 miles (19 km) of the US
coast, north of New York City. This was, however, rejected just
after the war by British authorities. Aviation historian Dr.
Kenneth P. Werrell states that the story of the flight
originated in two British intelligence reports from August 1944
which were based in part on the interrogation of prisoners, and
titled General Report on Aircraft Engines and Aircraft
Equipment; the reports claimed that the Ju 390 had taken
photographs of the coast of
Long Island.
These photos have never been discovered.
The claimed flight was mentioned in many books following the
RAF Flying Review account, including William Green's own
respected Warplanes of the Second World War (1968) and
Warplanes of the Third Reich (1970) but without ever citing
reliable sources. Further authors then cited Green's books as
their source for the claimed flight. Green himself told Kenneth
P. Werrell many years later that he no longer placed much
credence in the flight.
Werrell himself later examined the available data regarding the
Ju 390's range and concluded that although a
great circle round trip from France to
St. Johns, Newfoundland
was possible, adding another 2,380 miles (3,830 km) for a round
trip from St. Johns to Long Island made the flight "most
unlikely".
Karl Kössler and Günter Ott, in their book Die großen
Dessauer: Junkers Ju 89, 90, 290, 390. Die Geschichte einer
Flugzeugfamilie ("The Big Ones from Dessau...History of an
Aircraft Family"), also examined the claimed flight, and
thoroughly debunked the flight to Long Island. Most importantly,
it was nowhere near France at the time when the flight was
supposed to have taken place. According to Hans Pancherz'
logbook, the Ju 390 V1 was brought to Prague on
November 26, 1943. While there, it took part in a number of test
flights, which continued until late March, 1944. Secondly, they
also pointed out that the Ju 390 V1 prototype was unlikely to
have been capable of taking off with the fuel load necessary for
a flight of such duration due to strength concerns caused by its
modified structure; it would have required a takeoff weight of
72 tons, while the maximum takeoff weight during its trials had
been 38 tons. According to Kössler and Ott, the Ju 390 V2 could
not have made the US flight either, since they indicate that it
was not completed before September/October 1944.
General
characteristics
-
Crew:
10
-
Length:
34.20 m (112 ft 2 in)
-
Wingspan:
50.30 m (165 ft 1 in)
-
Height:
6.89 m (22 ft 7 in)
-
Wing area:
254 m² (2,730 ft²)
-
Empty
weight:
39,500 kg (87,100 lb)
-
Loaded
weight:
53,112 kg (117,092 lb)
-
Max
takeoff weight:
75,500 kg (166,400 lb)
-
Powerplant:
6×
BMW 801D
radial engines,
1,272 kW (1,730 hp) each
Performance
-
Maximum
speed:
505 km/h (314 mph)
-
Range:
9,700 km (6,030 mi)
-
Service
ceiling
6,000 m (19,700 ft)
-
Wing
loading:
209 kg/m² (42.8 lb/ft²)
-
Power/mass:
0.17 kW/kg (0.10 hp/lb)
Armament
-
Guns:
** 2 × 20 mm
MG
151/20
cannons
in dorsal turrets
-
1 × 20
mm MG 151/20
in
tail
-
2 × 13
mm
MG
131
machine guns
at waist
-
2 × 13
mm MG 131 in gondola
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