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Junkers Ju 87 Stuka

May 13th 1940, Junkers JU87 B-1s of 9/St.G 51 dive with sirens wailing onto French artillery positions in preparation for a full scale river crossing of the vital Meuse river barrier before Sedan. The banshee wailing of the infamous Stuka staffels brought the full psychological impact of the blitzkrieg to bear on the French defenders who broke and ran in the face of these terrifying attacks.

Country of Origin:

Germany

Manufacturer:

Junkers, Dessau (Ju 87A models and B-0)
Weser Flugzeugbau, Tempelhof (Ju 87B-1 onwards)

Major Variants:

Ju 87A, Ju 87B, Ju 87C, Ju 87D, Ju 87G, Ju 87H, Ju 87R

Role:

Dive-bomber, Ground and Armour attack, Trainer, Glider tug

Operated by:

Germany, Italy, Bulgaria, Hungary, Romania, Slovakia

First Flight:

Spring, 1935

In Service:

Luftwaffe, 1937, one Kette (3 aircraft) of StG 163 operational in Spain in Ju 87A-1s

Number Built:

5,709

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Overview

German and Chinese research into dive-bombing techniques using Junkers K47s during the mid-1920s led many Luftwaffe planners to consider this form of aircraft vital for combined-arms operations. When the Luftwaffe began expanding after 1933, a dive-bomber design was prominent. The general word for dive-bomber - Sturzkampfflugzeug - was shortened to become the name of the Ju 87, a Junkers low-wing monoplane design by Herman Pohlmann - the Stuka.

The first prototype flew in 1935 with a 640 hp Rolls Royce Kestrel engine. It had large fairings over its fixed main undercarriage, twin fins, full-length double-wing flaps and ailerons, two crew in a glass-house cockpit and dive brakes. The wing was an inverted gull-shape for strength and it also enabled more robust undercarriage. The tail assembly failed during dive-testing and was replaced with a strengthened single fin on the second and third prototypes as seen on all later production Stukas. After fitting a German 640 hp Junkers Jumo 210Ca engine with a three-bladed variable-pitch propeller, further testing lead to production of the A-1 model commencing in early 1937.

Production A-series Stukas were fitted with a 680 hp Jumo 210Da engine; a single 7.9 mm .311 in. MG 17 in the wing at the point of its bend; one 7.9 mm .311 in. MG 15 in the rear cockpit; and a bomb-load of one 551 lb 250 kg bomb. A single 1,102 lb 500 kg bomb could be lifted if crewed by the pilot only. A few were tested operationally during the Spanish civil war, but by the outbreak of World War II all A-series Stukas had been relegated to training schools.

The fitting of the 1,200 hp Jumo 211Da with fuel injection greatly improved the performance of the B-series. Fuel injection prevented negative-g flight and icing conditions from interfering with available engine-power, and the bomb-load was increased by the ability to lift an extra four 110 lb 50 kg bombs on wing racks over a short range. A second 7.9 mm .311 in. MG 17 was added to the other wing. An important addition was an automatic dive control device triggered by a contact altimeter which gave 450 m 1,476 ft of ground clearance during a six-g pull-out. Undercarriage spats were visibly altered by being made smaller and shaped around the wheels. B-series Stukas were involved in all early war operations and became the icon of Blitkreig.

C-series aircraft were planned for the aircraft carrier Graf Zeppelin and fitted with folding wings and an arrestor hook for deck operations, and flotation equipment and jettisonable wheels for ditching in water. When Graf Zeppelin construction was halted the C-models were completed and delivered as B-2 models.

About the same time, a long-range R-model was produced, and used successfully during the invasion of Norway. It had extra internal wing tankage and provision for under-wing drop tanks.

The most numerous of the Stukas produced was the D-series. It was introduced operationally in late 1941. The 1,400 hp Jumo 211J-1 engine and constant speed propeller enabled carriage of bomb loads of up to 1,800 kg 3,968 lbs, or a wide range of weapon-modules on under-wing racks. Defensive armament was increased to two 7.9 mm .311 in. MG 81z in the rear cockpit, and the D-7 and D-8 models had the internal wing guns replaced with 2 wing mounted 20 mm .75 in MG 151/20 cannon. By 1943 Stukas were being used primarily for ground attack and support and consequently protective armour was progressively added during D-series production. This added weight, and the D-7 was fitted with a 1,500 hp Jumo 211P engine. D-series aircraft were adapted for torpedo bombing, glider towing, night ground-attack, and various supply-pods for carriage of both men and equipment were experimented with. Production ended in September 1944.

An anti-armour version - the model G-1 - was created from converted D-5 model aircraft by attaching two 37 mm 1.5 in FLAK 18 cannon in underwing pods. This weapon was very successful in the hands of highly experienced pilots who could survive daylight operations with the now poor flight-performance of the Stuka. Hans Rudel claimed 519 Soviet armoured vehicles in 2,530 sorties, and was still flying a Ju 87G-1 in the Courland Pocket on the last day of the war. The specialist operational skills needed to survive Stuka operations in the late war period led to the H model, an unarmed dual-trainer with canopy bubbles in the rear for increased instructor visibility.

Hungary, Romania, Bulgaria, Slovakia and Italy were all provided with German-built Ju 87 Stukas. These aircraft mainly operated on the Eastern Front, although Italy also used Stukas in the Mediterranean theatre.

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Variants

Type

Number Built

Remarks

Prototype

3

First prototype with 640 hp Rolls Royce Kestrel liquid cooled engines, all metal stressed skin, inverted gull-wing, twin fins and rudders, a crew of two and dive brakes. Second two with 640 hp Junkers Jumo 210Ca engines with a three-bladed variable pitch propeller, and single fin and rudder.

Ju 87A-0

10

Pre-production aircraft; large-trouser undercarriage fairings; 640 hp Jumo 210Ca engines

Ju 87A-1

?

First production model; large-trouser undercarriage fairings; 640 hp Jumo 210Ca engines; one 250 kg 550 lb bomb (or 500 kg 1,102 lb as single-seater); 2 X 7.9 mm .31 in mg.

Ju 87A-2

total A 200

Large-trouser undercarriage fairings; 680 hp Jumo 210Da engines

Ju 87V-6

1

Test bed for 1,000 hp Jumo 211A engine; converted from A-1.

Ju 87V-7

1

Aerodynamically refined fuselage and wheel spats and 1,000 hp Jumo 211A engine as the prototype for the B series; converted from A-1.

JU 87B-0

10

Pre-production batch of the B model with the 1,000 hp Jumo 211A engine.

Ju 87B-1

?

First production B model with the Jumo 211Da engine developing 1,200 hp for take-off and featuring fuel injection preventing cut-outs under negative-g flight. Also automatic dive-control and pull-up. 3 X 7.9 mm .31 in mg.

Ju 87B-2

?

Improved production version; 1,000 kg 2,205 lb bombload as single-seater

Ju 87C-0

0

Carrier version for the Graf Zeppelin; folding wings; arrestor hook; jettisonable undercarriage; flotation equipment; aircraft all completed as B-1 models.

Ju 87R

?

Long range version; extra internal wing tanks and drop-tanks.

Ju 87D-1

?

Improved production version with 1,400 hp Jumo 211J-1 engine and broad-bladed propeller; bomb-load increased to 1800 kg 3,968 lb; wing racks able to carry various stores and gun-packs; fixed armament increased to 4 X 7.9 mm .31 in mg.

Ju 87D-2

?

Strengthened structure and glider-towing attachment added; converted from D-1

Ju 87D-3

?

Increased protective armour for greater ground-attack role.

Ju 87D-4

few only

Torpedo bomber

Ju 87D-5

?

Extended wingtips to counter increased weight; jettisonable undercarriage; dive-brakes deleted.

Ju 87D-7

?

night ground attack; night flying equipment; 1,500 hp Jumo 211P engine; flame-dampers; 2 wing mounted 20 mm .75 in MG 151/20 cannon; conv. from D-3 and D-5

Ju 87D-8

?

Final production version; day ground attack; as for D-7 without night equipment

Ju 87F

?

Projected version with revised aerodynamics and larger engine.

Ju 87G-1

?

Conversion of D-5 by addition of 2 X 37 mm 1.5 in FLAK 18 cannon underwing.

Ju 87H

?

Dual-control trainer; unarmed; rear-cockpit blisters for enhanced visibility

Ju 187

?

Further enhancement of the F model proposal; not built.

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Specifications

Model

Ju 87A-1

Ju 87B-1

Ju 87D-1

Ju 87D-7

Ju 87G-1

Dimensions

Span

45 ft 3.3 in
13.80 m

45 ft 3.3 in
13.80 m

45 ft 3.3 in
13.80 m

49 ft 2.5 in
15.00 m

49 ft 2.5 in
15.00 m

Length

35 ft 5.25 in
10.80 m

36 ft 5 in
11.10 m

37 ft 8.75 in
11.49 m

37 ft 8.75 in
11.49 m

37 ft 8.75 in
11.49 m

Height

12 ft 9.5 in
3.90 m

13 ft 2 in
4.01 m

12 ft 9.5 in
3.90 m

12 ft 9.5 in
3.90 m

12 ft 9.5 in
3.90 m

Wing area

343.37 sq ft
31.90 m

343.37 sq ft
31.90 m

343.37 sq ft
31.90 m

362.6 sq ft
33.67 m

362.6 sq ft
33.67 m

Powerplant

Type

Jumo 210Ca

Jumo 211Da

Jumo 211J-1

Jumo 211P

Jumo 211J-1

Cylinders

12

12

12

12

12

Horsepower

600

1,200

1,400

1,500

1,400

Weights and Loads (note - these figures vary for individual aircraft, and are often not directly comparable)

Weight (maximum)

7,495 lb
3,407 kg

9,560 lb
4,345 kg

14,550 lb
6,614 kg

14,565 lb
6,621 kg

14,550 lb
6,614 kg

Weight empty

5,104 lb
2,320 kg

6,090 lb
2,768 kg

8,598 lb
3,908 kg

8,683 lb
3,947 kg

9,700 lb
4,409 kg

Useful load

2,391 lb
1,087 kg

3,470 lb
1,577 kg

5,592 lb
2,705 kg

5,882 lb
2,674 kg

4,850 lb
2,205 kg

Performance (note - these figures vary for individual aircraft, and are often not directly comparable)

Maximum speed
at [height] mph kph

183 295
@ [9,840 ft]
[3,000 m]

238 383
@ [9,840 ft]
[3,000 m]

255 411
@ [13,500 ft]
[4,115 m]

248 399
@ [15,430 ft]
[4,703m]

195 314

Climb to height

-

3,716 m 12,190 ft 12 min

5,000 m 16,400 ft 19 min 48 sec

-

not known
extremely poor

Service ceiling

22,965 ft
7,000 m

26,250 ft
8,000 m

23,905 ft
7,286 m

-

not known
extremely poor

Range

620 ml
998 km

370 ml
596 km

954 ml
1,536 km

-

approx 450 ml
725 km

Armament

Armament

1 X 7.9 mm .311 in. MG 17 in wing
1 X 7.9 mm .311 in. MG 15 in cockpit
1 X 551 lb 250 kg bomb
[1,102 lb 500 kg if pilot only]

2 X 7.9 mm .311 in. MG 17 in wings
1 X 7.9 mm .311 in. MG 15 in cockpit
1 X 551 lb 250 kg bomb, and [short range only 4 X 110 lb 50 kg on wing racks].
[1,102 lb 500 kg if pilot only]

2 X 7.9 mm .311 in. MG 17 in wing
2 X 7.9 mm .311 in. MG 81z in cockpit
1 X 2,205 lb 1,000 kg bomb, or 1,102 lb 500 kg bomb and two weapons packs; or 3,968 lb 1,800 kg bomb [short range only]

2 X 20 mm .75 in MG 151/20 cannon in wing
2 X 7.9 mm .311 in. MG 81z in cockpit
1 X 2,205 lb 1,000 kg bomb, or 1,102 lb 500 kg bomb and two weapons packs; or 3,968 lb 1,800 kg bomb [short range only]

1 X 7.9 mm .311 in. MG 81z in cockpit
2 X 37 mm 1.5 in FLAK 18 in wing pods, or
1 X 2,205 lb 1,000 kg bomb

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