Heinkel He 219 Uhu / Letov LB-79

He 219A-0

The Heinkel Projekt 1060 private venture received little response from the Reichsluftfahrtministerium (air ministry) when it was first shown to them in mid 1940. It was a multi-purpose aircraft suitable for use as a long-range fighter, dive or horizontal bomber, torpedo plane, or reconnaissance aircraft. The He 219 featured tricycle landing gear, ejector seats, and dual wheels. It was equipped with a crew dingy, cockpit heating, retractable crew access ladder, armoured radiatios, armoured curved windshields with wipers, cleaing spray, hot air defrosting, and armoured fuel tanks. It had a complete wing, fuselage, and tail de-icing system, was well as elaborate radio and radar equipment including a directional gyroscope. Originally the Luftwaffe did not consider a craft of this type necessary and buried the project.

Heinkel He 219 Uhu Article

By late 1941 they were in desperate need of a good night fighter for intercepting Allied bombing attacks. In January 1942 the design was revised for adaptation as a night fighter but then was delayed by RAF bombing which destroyed all of the engineering drawings in the Heinkel factory at Rostock-Marienehe.

An all-metal shoulder-wing monoplane, the He 219 seated the pilot and navigator back-to-back, was the first operational aircraft in the world to introduce ejection seats, and was also the Luftwaffe’s first operational aircraft with tricycle landing gear. The first prototype, the He 219 V 1, powered by two 1305kW / 1750 hp DB 603A engines, made its first flight on November 15, 1942. The second prototype, flown in December 1942, had a different armament installation.

They proved fast and manoeuvrable, and had provision for a range of armament including two 20 mm (0.79 in) MG 151 cannon in the wings; two 30 mm (1.18 in) MK 108 cannon in a ventral tray; two oblique upward firing and fixed 30 mm (1.18 in) cannon, nicknamed ‘Schrage Musik’ (jazz music), in the rear fuselage; and a 2000-kg (4410 lb) bombload carried internally. The He 219 Uhu (owl) was a midwing monoplane and carried a crew of two.

Tests were so successful that the German Ministry ordered 130 pre-production machines in lieu of the usual ten.
General Milch, in charge of Luftwaffe procurement, was unimpressed with the He 219 and favoured converting existing types such as the Junkers 88 into night fighters. To determine the most suitable machine for nocturnal interception, comparative tests were set up for 25 March 1943 between the Heinkel He 219 and the Junkers Ju 88S. During a series of mock combats between a He 219 with Werner Streib at the controls and a Ju 88S with Oberst Lossberg in its cockpit, and a Dornier Do 217N, the 219 proved superior in every way. Heinkel soon received an order for 100 aircraft, and following evaluation of one of the prototypes in mock combat, an ‘off the drawing board’ order for 100 aircraft was increased to 300 by April 1943. Twenty pre-production He 219A 0s had been delivered by that time. These had slightly differing armaments, two MG 151s in the wings, with various weapons in the central position and only one MG 131 in the rear upper position.

The V4 V10 prototypes were also fitted with FuG 212 Lichtenstein C 1 radar systems.

The He 219A 0/R1 to /R6 were similar apart from modifications by Rustsatze (field conversion kits) which provided various ventral gun packs or MK 103 or MK 108 Schrage Musik cannon installations.

From April 1943 a small number of He 219A-0 pre-production aircraft flew with 1.NJG 1 at Venlo in the Netherlands, and on the night of 11 June 1943 Major Werner Streib shot down five Avro Lancasters in a single sortie. The first six operational sorties flown by the unit resulted in claims for 20 RAF aircraft, including six de Havilland Mosquitoes. Despite cancellation of the programme in May 1944, production deliveries of a number of versions were made, principally to 1./NJG 1 and NJGr 10.

He.219A-0 G9-FK of NJG 1

The main potential of the aircraft lay in the fact that it could compete on equal terms with the RAF Mosquito intruders. In late 1943 the He 219A-1 appeared, fitted with DB 603A or E engines plus GM1 power boost. Although it was proposed as a production model, only a few were built. The next main production model was the He 219A 2 with DB 603A engines and retaining the two MG 151s in the wings and the two Schrage Musik MK 108s; two MG 151s (A 2/R1) or MK 103s (A 2/R2) were mounted in the ventral tray. Forty of these were built. A proposed A 3 (three seat fighter bomber) and A 4 (Jumo engined high altitude reconnaissance bomber) did not get beyond the drawing board.

The calibre and number of cannon varied according to the armament available when each Heinkel left the production line. As a rule four 20mm or 30mm rapid fire cannon were located under the fuselage in a ventral tray and one 30mm cannon was installed in each wing root. In addition, two 30mm cannon were utilised mid-fuselage as upward-firing Schrage Musik. About one thousand rounds of ammunition were carried. All guns were located behind the pilot so that their muzzle flash would not disturb his vision at night.

Production continued in early 1944 with the A 5 which was characterized by a modified cockpit canopy. For this too there were various Rustsatze, RI to R3 denoting alternative ventral gun selections, and R4 providing a rearward firing gun operated by a third crew member. The A 5 series were powered by DB 603E, G or Aa engines. The A 6 was similar, but was re-engined with GM 1 boosted DB 603Ls of 2100 hp to increase its value as a Mosquito intercepter. The weight was reduced by retention of the wing and ventral armament installations only. Comparatively few A 6s were delivered.

The major service variant was the He 219A 7, a high altitude type powered by 1900 hp DB 603Gs, with increased armour plating and incorporating FuG 220 Lichtenstein SN 2 and FuG 218 Neptun radar equipment. More sophisticated radio systems were also installed. Alternative powerplants were used in the A 7/R5 (Junkers Jumo 213Es) and A 7/R6 (Junkers Jumo 222s). Armament of the A 7 series remained similar to that described and interchangeable, according to availability, using Rustadtze R1 to R4.

Yet another projected high altitude model, the He 219B-1 appeared in prototype form only. Based on an A 5 airframe, it had a longer fuselage, increased wing area and modified canopy, and carried a three man crew. A few B 2 anti Mosquito intercepters did serve with the Luftwaffe they were modified A 6s and a B 3 development was begun but not completed. Prototypes were also built of the He 219C 1 and C 2 night fighter and fighter bomber respectively. They had a redesigned fuselage to carry a four man crew, and with the ventral gun tray removed the C 2 could carry three 500 kg (1100 lb) bombs in its place.

Based on the success of the 219 during June 1943, General Kammhuber demanded the production of 1200 He.219 but General Milch fought the request which further delayed mass delivery. Finally Albert Speer took over the control of aircraft procurement and the Heinkel design was given priority status in early 1944.
A Fighter Emergency Program was announced in the Autumn of 1944. For reasons of economy all twin-engine fighter production was ordered halted, except for the jet powered Messerschmitt 262 and Dornier 335.
Heinkel ignored the directive and continued to produce 219 until his factories in Poland and Austria were overrun by the Russian Armies.

Six final aircraft were built from spare parts by staffel maintenance crews. These were secretly operated and their existence concealed from Luftwaffe headquarters.

Total overall production of the series was 294 aircraft. Early models were fitted with Daimler-Benz 603A engines of 1750 hp but the majority were powered by the more powerful Daimler-Benz 603-Gs of 1900 hp. There is no doubt that the He 219 was one of the best armed and most effective night fighters of the Second World War. Although the 219s did remain in service with the Nachtjagdgeschwadern (night fighter groups) until the end of the war, development of the type was discontinued in favour of two other designs both failures.

The first use of an ejection seat in combat came on 11 April 1944 when the two crew ejected from a Heinkel He219.

Letov LB-79 – Czech Air Force designation for two Heinkel He 219A-5 (lehký bombardér) built from recovered components, 1951, 1 (“34”) used as jet engine testbed.

Gallery

He 219
Engine: Daimler-Benz 603-G, 1900 hp
Weight: 33,730 lb
Fuel capacity: 293 gal
Maximum speed: 416 mph at 22,965 ft
Range econ cruise: 1243 miles at 335 mph
Climb to 32,810 ft: 18.8 min
Maximum ceiling: 41,660 ft

He 219A-0
Engines: 2 x Daimler-Benz DB 603A
Wingspan: 18.5 m (60 ft 8.5 in)
Length: 15.33 m (50 ft 11.75 in)
Height: 4.1 m (14 ft 5.5 in)
Weight empty: 11,200 kg (24,692 lb)
Combat weight: 27,661 lb
Max speed: 385 mph at 22,965 ft
Cruise: 295 mph
Ceiling: 41,660 ft
Range: 1243 miles
Armament: 2 x 30mm MG 151/20 cannon, 4 x 20mm MG 151/Mk 108/Mk 103 cannon, 2 x 20mm MG 151/Mk 108 cannon
Radar: FuG 220 Lichtenstein SN-2

He 219A 5/R2
Span: 18.5 m (60 ft 10.25 in)
Length: 15.54 m (50 ft 11.75in)
Gross weight: 13150 kg (28 990 lb)
Maximum speed: 630 km/h (391 mph).

He-219A-7/R1
Engine: 2 x Daimler-Benz DB 603G, 1417kW / 1874 hp
Max take-off weight: 15300 kg / 33731 lb
Empty weight: 11200 kg / 24692 lb
Wing loading: 70.52 lb/sq.ft / 344.0 kg/sq.m
Wingspan: 18.5 m / 60 ft 8 in
Length: 15.54 m / 50 ft 11 in
Height: 4.1 m / 13 ft 5 in
Wing area: 44.5 sq.m / 478.99 sq ft
Max. speed: 362 kts / 670 km/h / 416 mph
Cruise speed: 340 kts / 630 km/h / 391 mph
Ceiling: 12200 m / 40050 ft
Range: 1080 nm / 2000 km / 1243 miles
Armament: 4x MK 108 30mm, 2x MG151 20mm, 2x MK 103 30mm
Crew: 2

Heinkl He 177 Grief

The first prototype was flown in November 1939. It was a heavy bomber, introducing a power plant in which four Daimler-Benz DB 601 12-cylinder inverted engines were grouped together in pairs to create the DB 606, each pair driving a single propeller.

Many prototypes were built, most of which displayed obvious shortcomings including dangerous diving characteristics, landing gear and structural weaknesses, and problems associated with the engines including persistent crankshaft torsional vibration, lubrication and propeller troubles: two prototypes broke up in the air and at least one caught fire.

Heinkel He 177 Grief Article

Four years of development preceded the first production orders for the He 177.

Following a brief period of use as an emergency transport aircraft on the Eastern Front, during which time several caught fire and so earned the nickname “Flaming Coffin”. The first squadron of nine machines was sent to Stalingrad to supply the beleaguered fortress, but of the nine machines, seven caught fire and were burnt out.

The Greif began its operational career in October 1943 on anti-convoy and U-boat cooperation duties. It took part (sub-types A-3 and A-5) in attacks on England in January 1944, known as the “Little Blitz”, but as the war progressed was used to a greater extent as a missile carrier for anti-shipping duties. As the end of the war approached fewer and fewer Greifs remained operational: shortages of fuel and trouble with the engines grounding large numbers.

Although a small number of twin-finned He 177B were built in early 1944, most of the 1,160 or so Greifs produced were A-series types, although it is doubtful whether more than about 200 became fully operational in all respects. The He 177A-0 was the pilot production model, powered by two DB 606 engines (made up of four DB 601). Armament comprised two 13 mm MG 131 in dorsal and tail positions, one 7.9mm MG 81 in the nose, two 7.9mm MG 81 in a ventral position facing aft and a 20mm MG FF cannon firing forward from a “chin” position, plus 48x70kg, ten 500kg, six 1,000kg, or two 2,500kg bombs. The He 177A-1 was similar except for defensive armament, while the He 177A-3 had two DB 610 power units (four DB 603 engines), airframe changes and was equipped to carry two Hs 293 glider missiles. The final major version, the He 177A-5, was equipped to carry three Hs 293, two Hs 294 or two PC 1400 Fritz X (armour-piercing) radio-controlled missiles.

There were 40 modified He177 in Norway, May 1945 for a one way attack to USA.

A He 177 was intended for the continuance of the Me 264 steam turbine experiments. Later proposed designs had four separate engines which would have solved many of the problems, and was built as the He 277.

Gallery

He 177 A Greif
Length: 66.929 ft / 20.4 m
Height: 20.965 ft / 6.39 m
Wingspan : 103.15 ft / 31.44 m
Wing area : 1097.928 sq.ft / 102.0 sq.m
Max take off weight : 68355.0 lb / 31000.0 kg
Weight empty : 37044.0 lb / 16800.0 kg
Max. speed : 265 kts / 490 km/h
Cruising speed : 224 kts / 415 km/h
Service ceiling : 26247 ft / 8000 m
Wing load : 62.32 lb/sq.ft / 304.0 kg/sq.m
Range : 2970 nm / 5500 km
Engine : 2 x Daimler Benz DB 610 A, 2910 hp
Crew : 4
Armament : 3x MG 81 7,92mm, 3x MG 131 13mm, 2x MG 151 20mm, 1000kg Bomb. int., 2x HS293 Missl. ext.

He-177A-5/R-2
Engines: 2 x Daimler-Benz DB 610A/B, 2200kW
Max take-off weight: 31000 kg / 68344 lb
Empty weight: 16800 kg / 37038 lb
Wingspan: 31.44 m / 103 ft 2 in
Length: 20.40 m / 66 ft 11 in
Height: 6.39 m / 21 ft 0 in
Wing area: 102.0 sq.m / 1097.92 sq ft
Ceiling: 8000 m / 26250 ft
Range: 5500 km / 3418 miles
Armament: 3 x 7.92mm machine-guns, 3 x 13mm machine-guns, 2 x 20mm cannons, 1000kg of bomb
Crew: 6

Heinkel He 162

Originally scheduled for production in September, 1944, the Heinkel 162 was test flown for the first time just three months later. In such a desperate period it took just sixty nine days from the start of design work to its first flight.

Heinkel He 162 Article

The brief for the concept underlying the He 162 came from the Reichskriegsministerium (Ministry of War) who wanted fast, quantity production of a simple and effective jet interceptor as a last ditch air defence of the German homeland. Who originated the idea for what became known as the Volksjager (people’s fighter) is not clear. Albert Speer, the armament minister, is alleged to have been one of the promoters of the project, but Speer himself has said, somewhat evasively, that a proposal to establish an underground plant for the production of jet aircraft came from Fritz Sauckel, the gauleiter of Thuringen.
On September 8, 1944, the brief for the Volksjager was issued to the Arado, Blohm und Voss, Fieseler, Focke Wulf, Heinkel, Messerschmitt and Junkers companies. Strong opposition to the project was voiced by aircraft designers Willi Messerschmitt and Kurt Tank and General der Jagdflieger (general of fighters) Adolf Galland. In the opinion of these critics the construction specifications and conditions were unrealistic, but despite the protests the submission date for the draft projects was brought forward by approximately a week.
The specification stated that the design “had to make use of existing aircraft components, only the barest essentials to be carried in the way of equipment. The power to be supplied by a BMW 003 turbojet rated at 800 kg (1760 lb) st. Top speed to be 750 km/h (466 mph). Endurance of not less than 20 minutes at sea level. Gross weight not more than 2000 kg (4410 lb). Wing loading not more than 200 kg/sq m (41 lb/sq ft)”. These requirements were to be fulfilled with the use of readily available and, if possible, non essential mate¬rials. Unskilled and semiskilled labour was to be used on the production line. It is some indication of the desperation felt at this stage of the war that Hermann Goring, as commander in chief of the Luftwaffe, considered using Hitlerjugend (Hitler youth) members as pilots for the aircraft. Their initial flying training was to have been carried out on gliders before they converted to the jets.

A conference was held on September 15 to evaluate the submissions made by the aircraft manufacturers. Messerschmitt had refused to make a proposal, and of the others Arado’s was rejected, Focke Wulf’s was considered unrealistic (their participation had been for information purposes only), but the Blohm und Voss project was considered one of the best put forward. The Heinkel proposal was found deficient in five respects: it offered a sea level flight endurance of only 20 minutes; the unusual positioning of the engine would result in maintenance problems; the stipulated takeoff requirement had not been met; dismantling of the aircraft prior to rail transportation would take too long; and the 30 mm (1.18 in) armament specified in the brief had been changed to a 20 mm (0.79 in) cannon. After further conferences and discussions, one of which ended in a fierce quarrel between two of the participants, Heinkel were eventually authorized to produce the Volksjager and received the backing of Otto Saur, head of the war ministry’s Jagerstab (fighter staff), and Hermann Goring.
Since the early summer of 1944, Siegfried Gunter and Karl Schwarzler of Heinkel had been working on a project similar to the Volksjdger a small and simple jet fighter nicknamed Spatz (sparrow). Heinkel’s qualifications for producing the He 162, or Projekt 1073 as it was initially called, were further reinforced by their work in 1939 on the He 178 experimental jet and, a little later, on the He 280.

While some of the other companies barely had time to perform basic calculations for their designs, Heinkel had been working roughly along the same lines during the summer of 1944 and had test performance data on the BMW-003, along with a full scale mock-up of their concept.
There are allegations that Dr. Karl Frydag, head of the commission for airframe production and also a Heinkel company official, had not only sold the concept to Karl Saur, head of the Fighter Staff, but also may have let Heinkel know ahead of time of the upcoming specification.
A curious light is thrown on the situation by a document detailing a POW interview with a Flugbaumeister Halz of the Fl.-E-2 section of the Air Ministry that purports that when the decisive report on the Volksjäger concept was being sold to Göring, certain technical documents required to support their case were lacking and Halz was ordered to have faked photos of the He-162 with the help of a cinema expert, showing an He-162 prototype executing a roll above the clouds before a prototype was even built.

Construction of the He 162 began on September 24, 1944, with parallel work on the detailed drawings taking place. By September 30, Projekt 1073 had been ordered into quantity production with a pro¬posed monthly output of 500 to the Luftwaffe during the first thirty days of production, and eventually 1000 aircraft every month. When the drawings were completed on October 29, the first prototypes had already reached the advanced assembly stage. For the first time in aviation history, development, pre-production and series production of an aircraft occurred simultaneously.
The He 162 fuselage was of light metal flush-riveted monocoque construction, and was fitted with a moulded plywood nose cap. The single piece wing was made of wood and had a plywood skin, with detachable metal wing tips. The space between the wooden spars accommodated 40-gallon fuel cells. Four bolts held the wing to the fuselage mainframes. The metal flaps, which extend along the tapered trailing edge from the fuselage to the ailerons, have a maximum depression of 45 degrees with hydraulic motivation. Tailplanes, elevators and rudder were of light metal, but the fins were wooden. The narrow track tricycle landing gear was retracted hydraulically and lowered by springs. The aircraft was powered by a BMW 003 Sturm turbojet which was attached directly to the top of the fuselage immediately behind the cockpit by two vertical bolts at the forward end, and one horizontal bolt at the rear. The cockpit was equipped with an ejection seat designed by Heinkel.
The fuselage permits stowage of 168 gallons of fuel in the tail cone.
After October 30, 1944, all development and factory testing had to stop and effort was concentrated on full scale production. The first flight of the prototype took place on December 6, 1944. Although a main wheel door was torn off by the slipstream, the flight was in other respects considered successful. However, at an official demonstration four days later, the pilot was killed after the starboard wing broke up in mid air. Defective bonding of the wooden components was revealed as the cause. Nevertheless, pressure was put on the company for work to continue, and up to ten prototypes (He 162A 0s) and about 20 production aircraft were tested during December 1944 February 1945. The new aircraft, which was continually compared with the Me 262, was found deficient in many respects, including bad lateral stability, sluggish controls and a high roll to yaw ratio. Enlarging the fin area alleviated the first and third problems, and although the He 162 continued to suffer from a tendency to stall, this was eventually cured by applying a pronounced anhedral to the wingtips.
The facilities available for He 162 production were extraordinary, to say the least, varying from small carpentry workshops and chalk and salt mines to the renowned Sea Grotto near Vienna. There was only one main variant of the original design: the He 162A 2, armed with two 20 mm (0.79 in) MG 151 cannon positioned one on each side of the nosewheel well. The He 162A 3, like the A 1, mounted the heavier 30 mm (1.18 in) Mk 108 cannon originally specified, but this had to be abandoned since it caused too much vibration. Many other schemes included multibarrel projectile launch systems in the SGseries.

Despite the enormous numbers originally ordered, total production did not amount to more than about 275 aircraft and, so far as is known, I/JG1 was the only group to be fully equipped with the He 162 by the time Germany surrendered in 1945. During two weeks of flying ops, JG 1 (the main user of the He-162) were losing an average of one aircraft every two days due to flying accidents, pilot error, mechanical and structural failures. Operational testing had been carried out by Erprobungskorn¬mando (test detachment) 162 based at Rechlin, which after amalgamation with Adolf Galland’s famous Me 262 unit JV 44 in April 1945 was transferred to Salzburg/Maxglarn, where it was captured by the Americans on May 3. Other groups were partially equipped with the He 162 but because of lack of fuel and supplies it is unlikely that they saw any combat.
The production rate for the He 162 was to be 135 per day; Rostock Marienehe and Bernburg were each to deliver 1,000 per month and the vast underground Nordhausen Mittelwerke a further 2,000. Giant salt-mines were tooled up to make the BMW 003A turbojet, which was bolted above the light alloy fuselage of streamline profile, while the woodworking industry was harnessed to make the very small high mounted wing, only the down turned tips being metal. Armament was to be two 30 mm MK 108 cannon, but because of vibration these were replaced in production by two 20 mm MG 151s.
Development of the Heinkel He 162 led to the He 162C, with wing swept at 38 degrees and a butterfly tail. The He 162D was similar but featured a swept-forward wing. Neither version was built, but a model was found under construction with interchangeable wings when Schwechat was occupied by the Allies.
Many variants with different powerplants and equipment were tested by Heinkel in a desperate and futile effort to produce aircraft for the defence of the Third Reich in its last days. One of the most interesting was the Mistel 5 system in which the He 162 mothercraft was to carry a jettisonable Arado ¬powered bomb beneath the fuselage but this, like the others, did not come to fruition.
Only 140 had been completed by the end of the war.
Only two victories were claimed for the type during its short service life and both were unconfirmed.
After the end of the Second World War, He 162s were taken to Britain for study and evaluation, in the course of which another pilot lost his life in a crash landing at Farnborough. Three went to the US, and one to France where it is on display at the Musee de l’Air in Paris.

Musee de l’Air in Paris

Gallery

He 162 Salamander
Engine: One 1,760 lb. (800 kg.) thrust BMW 003A turbojet.
Wing span: 23 ft 7.75 in (7.2 m)
Length: 29 ft 8.5 in (9 m)
Height: 8 ft 4.5 in (2.55 m)
Max TO wt: 5953 lb (2700 kg)
Max level speed: 522 mph (835 kph) at 19,700 ft
Ceiling 39,500 ft. (12,000 m.)
Climb rate 4,200 fpm at sea level
Fully loaded Range 410 miles (660 km.)
Endurance: 45 min
Armament 2 x 30 mm MK-108 or MG-151 cannon.
Take off distance 875 yards
Take off distance JATO 415 yards

He 162A 2
Engine: one 800 kg (1,764 1b) thrust BMW 109 003E 1 or E 2 turbojet.
Max speed: 835 km/h (519 mph) at 6000 m (19,685 ft)
Initial climb rate 1290 m (4,230 ft) per minute
Service ceiling about 11000m (36,090ft)
Max range 1000 km (621 miles)
Empty wt: 1750kg (3,8581b)
MTOW: 2700 kg (6, 952 lb)
Wing span 7.20 m (23 ft 7.5 in)
Length 9,05 m (29 ft 8.5 in)
Height 2.55 m (8 ft 43/8 in)
Wing area 11.15sq.m (120.0 sq.ft)
Armament: two 30 mm MK 108 or two 20 mm MG 151 cannon in nose.

He 162 A-2 Salamander / Volksjäger
Engine : BMW 003 E-1, 7848 N
Length : 29.659 ft / 9.04 m
Height : 8.497 ft / 2.59 m
Wingspan : 23.622 ft / 7.2 m
Wing area : 120.557 sq.ft / 11.2 sq.m
Max take off weight : 5931.5 lb / 2690.0 kg
Weight empty : 4520.3 lb / 2050.0 kg
Max. speed : 452 kt / 838 km/h
Service ceiling : 39370 ft / 12000 m
Wing load : 49.2 lb/sq.ft / 240.0 kg/sq.m
Range : 526 nm / 975 km
Endurance : 1 h
Crew : 1
Armament : 2 MG 151 20mm

Heinkel He 115

Design of this large seaplane started in 1935 as a faster and more manoeuvrable replacement for the He 59.
It was an all metal mid wing monoplane with single step metal floats. For its size it handled well and gave good performance.

Heinkel He 115 Article

The prototype He 115 V1 (D AEHF) was first flown in August 1937, powered by two 800 hp BMW 132K nine cylinder radials. After further flight trials its two machine-guns were then removed, their positions faired over, and on 20 March 1938 the aircraft set eight payload/speed records.

This aircraft was followed by three more prototypes of which the He 115 V3 (D ABZV) was the first aircraft to be given the extensively glazed nose of the final production version. The field of view for two of the three man crew was increased still further by extended glazing of the canopy from the cockpit back to the mid-¬fuselage position. The fourth prototype was the production prototype with float/ fuselage bracing wires replaced by struts.

An evaluation batch of ten, designated He 115A 0, also produced in 1937-38, were followed in 1939 by 34 He 115A 1s, powered by uprated 960 hp BMW 132K engines. The He 115A 0s were armed with a single 7.9 mm (0.311 in) machine gun in the extreme nose while A 1 models were fitted with an extra MG 15 gun and were used as torpedo attack aircraft. Some A 1s were built for export and designated A 2: Norway bought six and Sweden 10.

The first large scale production version for the Luftwaffe derived from the V5 (itself modified from an A 0) which developed into the He 115B series. These aircraft had structural improvements to accommodate the heavier payload, an increased fuel capacity, and provision for up to five 250 kg (550 lb) bombs. Alternatively, two 250 kg (550 lb) bombs and an 800 kg (1760 lb) or 920 kg (2030 lb) torpedo or mine could typically be carried. Manufacture continued until 1944, by which time production totalled 138 air¬craft, excluding prototypes.

The B series was followed by the He 115C series, begun in 1940 and entering Luftwaffe service the following year. The C 1 had an additional under nose MG 151 cannon and two rearward firing MG 17 machine guns mounted in the rear of the engine nacelles. Subsequent C variants were generally similar, the C 2 having reinforced floats; the C 3s were fitted with mine-laying equipment; and the C 4s were used as torpedo bombers, armed with only three rearward firing machine guns.

A one off He 115A 1, converted to become the He 115D, was armed with one cannon and five machine guns, carried a fourth crew member, and was powered by two 1600 hp BMW 801MA radial engines. It was used operationally but did not go into series production.

The He 115 stayed in useful service until 1944, and was used mainly in Scandinavia, the North Sea and English Channel, the north of Germany, and to a lesser extent in the North African and Mediterranean theatres. Two of the Norwegian He 115A 2s escaped to the UK in 1940 and, together with an ex-Luftwaffe B-1, were used by the RAF to carry agents between Malta and North Africa. During their service lives, the He 115B and C models were fitted with a variety of Rustsatze (field conversion kits) comprising variations in the nature of the operational payload carried. The particular kit was indicated in a suffix to the main designation: thus, for example, the He 115B-1/R1 was a standard B-1 carrying a photo reconnaissance twin camera installation (R1), whereas the He 115B 1/R3 was equipped with one 920 kg (2030 lb) or two 500 kg (1100 lb) aerial mines and their release gear.

Gallery

He 115C-1
Engines: 2 x BMW 132K, 960 hp / 872 kW
Span: 22.3 m (73 ft 2 in)
Length: 17.3 m (56 ft 9 in)
Height: 21 ft 7.25 in / 6.59 m
Wing area: 933.23 sq.ft / 86.70 sq.m
Empty weight: 15,146 lb / 6870 kg
Gross weight: 10680 kg (23550 lb)
Maximum speed: 300 km/h (186 mph) at 3280 ft / 1000m
Climb to 3280ft/1000m: 5 min 6 sec
Service ceiling: 18,040 ft / 5500m
Range: 1740 mi / 2800 km
Seats: 3
Armament: 1 x 15mm cannon / 4 x 7.92mm mg
Bombload: 2756 / 1250 kg or 1 x 1102 lb / 500 kg torpedo

Heinkel He 114

He 114A

Begun by Heinkel under Luftwaffe contract at the beginning of 1936, the first of five variously ¬powered prototypes flew in the late spring of that year. It was a two seat, all metal two float seaplane of sesquiplane configuration, fitted with a 960 hp DB 600A engine driving a three blade wooden propeller.

The five prototypes, flown in 1936 and 1937, were powered by a variety of engines, including the 716kW Daimler-Benz DB 600, the 477kW Junkers Jumo 210, the 656kW BMW 132Dc and the 716kW BMW 132K.

These five, and the first of ten pre-production He 114A-0s, were delivered to the Luftwaffe during 1937, with the BMW 132Dc engine, which was adopted also for the 33 He 114A-1 trainers, though they were neither armed nor fitted with catapult hooks. Thirty three 865-hp BMW-132N engined A 1s were built as trainers by Weser.
Earlier that year the German aviation ministry accepted the V9 (D IHDG) as prototype for the He 114A 2 series, which were powered by an uprated (960 hp) BMW 132K engine driving a three blade constant speed propeller and fitted with catapult gear. It flew for the first time on February 16, 1937 and a small batch of A 2s, again built by Weser, were delivered to the Luftwaffe later in the year. The He 114A-2 was the first operational version, armed with a fixed forward-firing 7.92mm MG 17 machine-gun and an identical weapon mounted in the observer’s cockpit.

They were equipped with catapult points and could carry two 50 kg (110 lb) bombs. The Luftwaffe pilots found their handling on the water and in the air to be somewhat unstable, and the He 114 never superseded the He 60 in service. The prewar A 2s were later converted by Weser for export to Sweden (14 as He 114B 1s) and Romania (six He 114B-2 aircraft, three with DB 600 engines and three with Jumo 210s). Romania also bought 12 He 114B-2S with BMW 132K engines.
14 He 114A-2s were exported to Sweden as the He 114B-1.
Fourteen He 114C 1s were used by the Luftwaffe as commerce raiders, and four unarmed C 2s were delivered for use as trainers in December 1939, having the 865 hp BMW 132N engine. At the outbreak of the Second World War, the C l s and some other models were equipped with one or two additional MG 17 machine guns in the pilot’s cockpit, firing past the propeller. Some He 114s carried four 50 kg (110 lb) bombs for antisubmarine duties (only two when additional machine gun armament was carried). The He 114 was phased out during the first two years of the war, after limited Luftwaffe service.
Production ceased in 1939.

He 114A 2
Engine: 1 x BMW 132K, 610kW
Wingspan: 13.6 m (44 ft 7.5 in)
Length: 11.65 m (38 ft 2.75 in)
Height: 5.2 m / 17 ft 1 in
Wing area: 42.3 sq.m / 455.31 sq ft
Max take-off weight: 3420 kg / 7540 lb
Empty weight: 2314 kg / 5102 lb
Max. speed: 292 km/h / 181 mph
Cruise speed: 265 km/h / 165 mph
Ceiling: 4800 m / 15750 ft
Range w/max.fuel: 1050 km / 652 miles
Range w/max.payload: 910 km / 565 miles
Armament: 1 x 7.92mm machine-guns
Crew: 2

He 114

Heinkel He 112 / He 113

He 112B

Shortly after the Nazi party came to power in Germany in 1933 a requirement was issued for an up to date single seat monoplane successor to the He 51 and Arado Ar 68 biplanes. Heinkel’s designers chose the comparatively easy task of refining the He 70 configuration to produce the He 112, which had an open cockpit, all metal fuselage and elliptical wings. The prototype VI (D IADO) was powered by a 518kW / 695 hp Rolls Royce Kestrel V engine and flew for the first time in late summer 1935. It was flown to Travernfinde for official tests in October that year, competing with the Arado Ar 80, Focke Wulf Fw 159 and Messerschmitt Bf 109.

Both it and Messerschmitt’s Bf 109 received orders for 10 aircraft.

November and December 1935 saw the appearance of second and third prototypes (V2 and V3), both later having the wing span reduced by 1 m (3 ft 3 in) and powered by 447kW / 600 hp Junkers Jumo 210C engines. The V3 was armed with two 7.9 mm (0.311 in) MG 17 guns mounted over the nose, and had an enclosed cockpit.

The He 112 V4, V5, V6 and V8 were built as prototypes for the projected He 112A production series.

The fourth prototype, He 113, with a new, smaller, elliptical wing, was evaluated operationally with the Legion Condor in Spain in 1936, and was shown at the July 1937 Zurich International Flying Meeting.

He 113

The V8 was tried with a 1000 hp DB 600Aa powerplant, but no A series production order was received although the aircraft was well liked by its pilots.
The proposed He 112A production aircraft was not adopted by the Luftwaffe, which received the Bf 109 instead, but work continued on the structurally-redesigned He 112B, the 507kW Jumo 210Ea-powered production prototype which flew in July 1937.

A batch of 43 He 112B 0s was, however, produced, based on the much modified V7 and V9 prototypes. Armament comprised two MG 17s, which were now fitted in the fuselage sides, plus two wing mounted 20¬mm (0.79 in) MG FF cannon. Powerplant was the 680 hp Junkers Jumo 210Ea 12-cylinder liquid cooled engine. In spring 1938 Japanese naval aviation had also received 12 of 30 He 112B 0s ordered in the spring of 1938 but pilots were not enthusiastic and the aircraft were used mainly for ground instruction; their Japanese designation was A7He1. They received the allied code name ‘Jerry’ although this was dropped when not met in combat.

A7He1

The next 12 were impressed for Luftwaffe use, although 11 of these and the final six were supplied later to the Spanish Nationalist air force in November 1938. Deliveries of 12 to the Luftwaffe commenced in mid 1938 for service trials, and later that year 17 flew with the rebel Spanish Nationalist forces in Spain. Fifteen survived the civil war to serve with the new Spanish air force in Morocco.

Hungary acquired the V9 and three B Is for evaluation in the spring of 1939, and the only other buyer for the He 112 was Romania, which ordered 24 (13 13 0s and 11 B 1s) , the order being completed in September 1939. They served briefly during the Second World War, the only He 112s to do so.
In the fighter bomber role the aircraft could be fitted with underwing racks to carry six 10 kg (22 lb) antipersonnel bombs. Two further prototypes, the V10 and V11 with DB 601Aa and Junkers Jumo 210G engines respectively, were produced in the hope of encouraging further export orders, but none were forthcoming and Heinkel decided to use its workforce on producing types acceptable to the Luftwaffe.
In 1937 one He 112 was fitted with an experimental 2200-lb thrust liquid-fuel rocket motor in its tail. This led to the He 176 of 1938.

Rocket powered He 112

He 112B
Span: 9.1 m (29 ft 10.25 in)
Length: 9.3 m (30 ft 6 in)
Gross weight: 2250 kg (4960 lb)
Maximum speed: 510 km/h (317 mph)
Armament: 2 x 20mm MG FF cannon, 2 x 7.92mm MG 17 machine-guns

He-112B-1
Engine: 1 x Jumo 210G, 490kW
Max take-off weight: 2250 kg / 4960 lb
Empty weight: 1850 kg / 4079 lb
Wingspan: 9.1 m / 29 ft 10 in
Length: 9.3 m / 30 ft 6 in
Height: 3.9 m / 12 ft 10 in
Wing area: 17.0 sq.m / 182.99 sq ft
Max. speed: 510 km/h / 317 mph
Cruise speed: 475 km/h / 295 mph
Ceiling: 9500 m / 31150 ft
Range w/max.fuel: 950 km / 590 miles
Range w/max.payload; 850 km / 528 miles
Armament: Armament: 2 x 20mm MG FF cannon, 2 x 7.92mm MG 17 machine-guns
Crew: 1

He 113
Engine: Mercedes-Benz DB601, 1200 hp
Span: 30 ft 11 in
Length: 26 ft 7 in
Height: 8 ft 2 in
Max speed: 375 mph
Armament: 1 x cannon, 2 x mg

He 112

Heinkel He 111

From the beginning, the He 111 was designed to fulfil the roles of both bomber and commercial aircraft. There were no basic structural differences between these two versions. Walter and Siegfried Gunter began work on the design of this all metal low wing monoplane in early 1934. The first prototype, the He 111 VI, appeared at the end of that year as an extremely clean looking and efficient aeroplane. Powered by two 447kW 660 hp BMW VI 6, OZ glycol-cooled inverted V engines, it was flown for the first time on February 24, 1935. It was equipped as a medium bomber, with provision for a 1000 kg (2200 lb) internal load of bombs (which were stowed upright), and had an armament of three 7.9 mm (0.311in) MG 15 machine guns: one each in nose and dorsal positions and one in a retractable ventral ‘dustbin’.

Heinkel He 111 Article

The wings were of semi-elliptical planform, fitted with hydraulically operated trailing-edge flaps, the tailwheel-type retractable landing gear also being hydraulically actuated. Very clean in appearance, the prototype (in bomber configuration) was able to accommodate an internal bomb load of 1,000kg, and was armed with three machine-guns in nose, dorsal and ventral positions. Flight testing proved that its performance equalled or even bettered that of contemporary fighters.

Of the new three prototypes, the V2 (D-ALIX) and V4 (D AHAO) were built as commercial transports, with accommodation for ten passengers and a cargo of mail. Heinkel tried to interest Deutsche Lufthansa in the He 111 as a commercial transport, and the idea that it was purely a civil type was fostered by the German government even after the existence of the military version officially became known in January 1936.
The second prototype was completed as a civil transport and was handed over to Luft-Hansa following the termination of early testing. Subsequently, this aircraft reverted to being used by the Luftwaffe for secret high-altitude reconnaissance missions. Many such missions were flown prior to the outbreak of World War II, both by military and civil aircraft, so that long before wartime operational missions were flown, the Luftwaffe had acquired very detailed documentation of a vast number of important targets.

The fourth prototype, with accommodation for ten passengers in two cabins, named Dresden, was delivered to Luft-Hansa on 10 January 1936 by Heinkel’s test pilot Gerhard Nitschke. Six production airliners, He 111C named Breslau, Karlsruhe, Koln, Konigsberg, Leipzig, and Numberg, entered service from the summer of 1936.

Lufthansa did in fact operate small numbers of the He 111C and He 111G, but not until some time later. The V3 (D ALES) was the prototype for the first military version, and ten pre-production He IIIA 0s were constructed towards the end of 1935 at Rostock-Marienehe and delivered to the Rechlin test centre of the Luftwaffe during the spring of 1936. It inherited the elegant lines of its single engined forebear, the He 70, and had generally good handling characteristics, but the BMW engined He 111 was found to be insufficiently powerful for military use. The Luftwaffe therefore rejected the similarly powered He IIIA Is that had been completed, and the pre-production A 0 machines were sold to China.

The He 111A initial bomber variant was underpowered and lacked adequate performance, but this was rectified in the He 111B series by a switch from the 492-kW (660-hp) BMW 6,0Z to the Daimler-Benz DB 600, which not only boosted performance but also permitted the carriage of a heavier warload.

The first Luftwaffe versions, therefore, were the He 111B 0 and B 1, based on the He 111 V5 prototype (D APYS) and powered by DB 600A or C engines. B 1 deliveries to Kampfgeschwader (bomber group) 154 began in late 1936, followed in 1937 by the He 111 B2 which was powered by 950 hp DB 600CG engines and carried a short range bombload of 1500 kg (3310 lb). As with so many other Luftwaffe aircraft types of the period, the B2 was deployed by the Legion Kondor in Spain in early 1937, soon meeting with considerable combat success against the government forces. It gained a reputation of having the speed to outrun most enemy intercepters, which enabled it to operate without a fighter escort. (The He 111B 1, with 950 hp DB 600Ga engines, was faster than the B 2, but was built only in very small numbers and was not used operationally.)
The type was soon slated for evaluation with Kampfgruppe 88 of the Legion Condor, and from February 1937 some 30 He 111B-1/2s were despatched for service with two of KG/88s three Steffeln.

Production of He 111 bombers continued with the He 11IE, although this had been preceded by the second major civil variant, the He 111G. This latter model did not attract many customers, but it was noteworthy in having introduced a redesigned wing with straight taper, which was easier to produce than the semi elliptical shape that characterized the previous models. The He IIIE retained the original wing form, but introduced another basic change the adoption of the Junkers Jumo 211 engine (in this series the 1010 hp Jumo 211A 1) in order to pre¬serve supplies of the DB 600 for fighter production. Sub types of the E series included the E 1, with 2000 kg (4410 lb) internal bombload; the E 3, similar except for equipment changes; and the most numerous E model, the E 4, which could carry 1000 kg (2200 lb) internally and equal load externally; and the E 5, with additional fuel tanks.

The type proved very successful in operational and maintenance terms, and from March 1938 some 45 He 111 E-1 s with a heavier warload were despatched for service with KG/88s four Staffeln, the He 111B-1/2s being passed to the Nationalists 10- and 11-G-25. At the end of the war the 58 surviving He 111s were given to Spain.
The ‘straight’ wing was combined with the slightly more powerful 1100 hp Jumo 211A 3 to produce the He 111F, the prototype of which appeared in mid 1937. He 111Es also served in Spain and the combined total of Bs and Es sent to Spain was 75, of which 58 survived the civil war to form a part of the reconstituted Spanish air force. The main Luftwaffe F model was the He 111F 4. Exports at this time included 24 He 111F Is and five He 111G 5s to the Turkish air force.

One other Luftwafte variant with DB 600 engines was the He 111 J (with DB 600CGs), about 90 of which were completed. They were otherwise generally similar to the F 4, except that their bomb bays were deleted as they were intended for use as torpedo-bombers though they were, in fact, delivered for service on standard bombing duties.

The second generation He 111 bomber mated the entirely new wing introduced by the first generation He 111F and J with a completely revised forward fuselage. A major design change, one which gave the He 111 quite literally a new look, occurred in the He 111P, which began to enter service during the early part of 1939. This took the form of a complete redesign of the fuselage nose, eliminating the conventional ‘step’ created by the pilots’ flight deck windows in favour of an extensively glazed forward section which maintained the flow of the fuselage lines unbroken above and below the nose. The pilot was seated to port and all flight and engine instruments were mounted on a panel suspended from the roof.

Provision was made for elevating the pilot’s seat and controls for landing and taxying, his head projecting through a sliding panel and being protected from the slipstream by a small retractable windscreen. Although the cockpit glazing was criticised for mirror effect in aft sun, the new forward fuselage was standardised for subsequent production, these beginning to leave assembly lines in the winter of 1938-39.

At the tip of this new nose, and offset to starboard, was a ball type Ikaria universal mounting for the nose 7.9mm MG 15 machine gun. The P series comprised the P 1 and P 2, which differed only in their radio equipment; the P¬3, a conversion for dual control training; and the P 4 and P 6.

The He 111P-4 introduced some armour protection for the pilot and dorsal and ventral gunners, and heavier defensive armament, this being six 7.9mm MG 15s. The port bomb bay was blanked off and occupied by a supplementary fuel tank, bomb racks being introduced beneath the blanked-off bay.

Overall He 111 P production, shared by Arado, Dornier and Heinkel, was in the region of 400 aircraft. Early models had 1100 hp DB601A engines, three defensive machine guns, and the standard 2000 kg (4410 1b) bombload carried half internally and half externally. Need for better defence was reflected in the armour protection of the P 4 and P 6, the former also mounting up to six MG 15 machine guns (and, sometimes, an MG 17 in the tail). The P 6 (there was no P 5 built) was similar to the P 4 except for 1175-hp DB 60IN engines ten of this model were supplied in 1942 to the Hungarian air force.

Whereas the original wing had been of elliptical form, its complex structure inhibited large-scale production. Early in 1936 Siegried Günter began redesign of the wing, eliminating the ellipses in favour of a straight tapered planform, reducing the wing area in the process. Comparatively small numbers were completed with the new wing before, in the Summer of 1938, and entirely new forward fuselage was introduced on the assembly lines.

He 111P-6

Like other earlier models, however, the He 111P was drawing upon supplies of engines more urgently needed for fighter production, and so relatively few of this series were built.

The second generation bomber had been planed to take either Daimler-Benz DB 601A or Junkers Jumo 211 engines, The He 111P with the Daimler-Benz and the He 111H with the Junkers. Priority was given to the DB 601A-engined version owing to the supply situation.

Deliveries of the initial production model, the He 111P-1, began during the early spring of 1939, the first He 111H-1s following six weeks later. The H-1 being equipped to a similar standard with deliveries commencing in the same month (May).

The next model to enter production, and the most numerous of all, was the He 111 H. This combined the airframe of the early P models with the Jumo 211 powerplant. By the time He 111 production was phased out in the autumn of 1944 well over 7000 had been turned out, of which more than 6000 were sub types of the H series. Power plant of the He 111H comprised two Junkers Jumo engines, with power ranging from 752.6kW for the Jumo 221A to 1,323.5kW in the Jumo 213A-1 installed in the final production He 111H-23 paratroop carrier.

Production of the P-series was to be finally phased out early in 1940 with the He 111P-6, this reverting to the standard internal bomb stowage arrangement but having 1275 hp DB 601N engines. The He 111H-2 had similar armament to the P-4, the He 111H-3, which appeared in November 1939, being a dual-role version adding anti-shipping operations. The H-3 was fitted with a single forward-firing 20mm MG FF cannon in its ventral gondola. The H-3 had Jumo 211D-1 engines of 1200 hp for takeoff. These engines were retained initially by the He 111H-4 which began to come off the lines early in 1940, but were eventually to be supplanted by the Jumo 211F-1 of 1400 hp for takeoff.

By the beginning of WW2 the He 111-equipped Kampfgeschwader had virtually completed conversion to the second generation bomber which comprised the bulk of the equipment of 21 Gruppen and one Staffel with a total strength of 789 aircraft.

One shortcoming of the second generation He 111 was its inflexibility concerning bomb loading arrangements. The bombs were loaded into individual vertical cells, four on each side of the gangway, and this meant that the largest bomb that could be accommodated internally was a 551 lb / 250 kg. There was no increase in defensive armament which remained three 7.9mm MG 15 machine guns. The crew comprised pilot, navigator/bombardier, radio operator and ventral gunner. The DB 601A-1 engines of the He 111P were each rated at 1175 hp for takeoff and the Jumo 211A-1 engines of the He 111H each were 1075 hp for takeoff.

The He 111P was built by Heinkel’s Rostock-Marienehe and the NDW factories, these being joined by Arado at Warnemünde, while the He 111H was built in parallel by Heinkel’s Oranienburg facility, the Junkers plant at Dessau and the new ATG factory at Leipzig.

He.111H

Production of the He 111 had reached almost 1000 by the start of the Second World War, at which time 349 of those in Luftwaffe service were He 111Ps and 400 were He 111Hs of one model or another, all having been taken on charge over a period of less than six months.

It did not take long to destroy the illusion of security created by their easy passage during the Spanish Civil War. Committed to the Polish Campaign, the He 111 achieved generally favourable results, but attrition was higher than anticipated, a total of 78 bombers being lost.

For the onslaught on France and the Low Countries on 10 May 1940, Luftflotten 2 and 3 possessed a total of 1120 twin-engined bombers of which approximately half were He 111s. By then Kampfgruppen were converting to the Junkers Ju 88A. By Adler Tag only four Kampfgeschwader remained completely equipped with He 111s, these being KG 26 based in Norway, KG 27 operating from Tours, Dinard and Rennes, KG 53 at Lille-Nord and KG 55 at Chartres, Dreux and Hillacoublay.

After initial strikes across the Straits of Dover, the first sorties in force by He 111s took place on 15 August when 72 He 111H-4s of I and III Gruppen of KG 26 flew from Stavanger with the intention of attacking RAF bases at Dishforth, Ulswortg and Linton-upon-Ouse. The bomber force was escorted by Bf 110 fighters of I/ZG 76, but owing to a navigational error none were to find their target. Only 63 of the He 111s actually crossed the coast and eight fell to RAF fighters. Despite heavy operational attrition, daylight attacks by He 111 formations against the UK continued for a month.

The provision of Bf 109E fighter escorts barely alleviated the situation. From 16 September the He 111 was to be largely confined to nocturnal sorties.

After experience of rough handling by the RAF’s Hurricanes and Spitfires during the Battle of Britain, moves were soon under way to increase the bomber’s defensive armament. This began with the addition of two 7.9 mm (0.311in) beam guns on the He 111 H 2; other typical variations in armament included the provision of a 20 mm (0.79 in) MG FF cannon in the under nose gondola of some H 3s, for anti-shipping attacks (Up to 2000 kg (4410 1b) of bombs could be accommodated); a combination of one MG FF, one 7.9 mm (0.311 in) MG 17, and either one 13¬mm (0.51 in) MG 131 or two 7.9 mm (0.311¬in) MG 81 guns on the H 10; and four MG 81s and three MG 131s on the He 111 H 20. In all, there were 23 sub types of the H series, of which the most numerous models were the H 3, H 6 and H 16. Most H sub types were powered by successive versions of the Jumo 211 engine, although the H 21 had 1750 hp Jumo 213Es and the H 23 was fitted with 1776 hp Jumo 213As.
With such numbers available, it was inevitable that the He 111 should be called upon to undertake a wide variety of duties in addition to the standard bombing role. The H 3 and H¬6 became excellent anti-shipping aircraft, the latter becoming operational in the spring of 1942 and being able to carry bombs or mines internally and two externally slung torpedoes. A large fender to cut through or push aside the cables of barrage balloons was fitted to the He 111H 8. The H 10 and H 18 were night bombers; the H 12 was adapted as a carrier for a pair of Henschel Hs 293 glider-bombs; the H 14 served both as a pathfinder bomber and a glider tug; the H 15 was a carrier aircraft for Blohm und Voss glider-bombs; the H 22 was the version adapted as air launch aircraft for Fieseler Fi 103 (V1) flying bombs; and the final model, the He 111 H 23, was an assault or saboteur transport carrying eight paratroops.

He 111H-22

By 1 September 1944 the last of the ground launch ramps for the V-1s had fallen into Allied hands, so the Luftwaffe stepped up the use of He 111s as V-1 launch ramps. Soon more than 100 aircraft were being used on these missions, including a number of Heinkel He 111H-21s with powerful Jumo 221 engines. After brief training at Peenemunde and Oschatz, the 3rd Group of the German ‘Blitz Wing’ (3rd Bomber Wing) became 1st Group of the 53rd Bomber Wing (‘Condor Legion’) and started operations in mid-July 1944. The planes took off with their flying bombs from Dutch bases at Venlo and Gilze Rijen. By the start of September, large numbers of V-1s had been launched from He 111s, of these, 30 had landed in London, 90 in Southampton, and more than 20 in Gloucester.
To avoid the powerful British anti-aircraft, most of the He 111 missions had to be carried out at night; the bomber also had to fly at low altitude in order to stay underneath the British radar screen. When they came within 35 miles of the British coast, they climbed to about 1500 ft, launched their V-1s and headed back to the Continent, flying just above the water’s surface.
Operation Rumpelkammer, the German program to launch V-1s from aircraft, cost many casualties, for often the flying bombs would explode while taking off from the carrier plane.

By the end of September 1944, the He 111s of the 1st Group had fired a total of 177 flying bombs at England, mostly in night missions. 1st Group were now taking off from their new bases in Schleswig-Holsstein, Oldenburg and northern Westphalia. The German aircraft suffered heavy losses on V-1 launch missions. In one instance, 12 He 111s failed to return from two successive missions, after RAF night fighters and explosions after take-off.
On Christmas Eve 1944, aa group of He 111s of 1st Group took off on a V-1 raid against Manchester. One of the flying bombs crashed over the city and 17 others went down within a 15-mile radius.
At 4:30am on 14 January 1945, a V-1 exploded near Hornsea, Yorkshire. It was the last of some 1200 flying bombs launched from the air by Heinkel He 111 bombers of 1st Group, 53rd Bomber Wing. Only one out of ten V-1s came close to hitting its target; the rest fell victim to the Allied air defence or crashed prematurely dur to faulty guidance systems.

At noon on 8 May 1945, two Soviet fighters flown by G.A. Lobov, the commander of the Seventh Guard Division, and by Capt. Svidirov, ran into a solo-flying He 111 and shot it down. This ended the operations of Soviet fighters in the air war over Europe.

Although it was thought that Aichi produced radial powered He.111K under licence as the Type 98, the type never existed. One 1942 military recognition manual still stated a very few He.111s have been met in action.

The Heinkel He 111 Zwilling (Twin) consisted of two Heinkel He 111H-6 twin-engined medium bombers joined together. Created by ‘marrying’ two standard He 111H 6s or 16s by connecting them with a new wing centre section which mounted a fifth Jumo 211F-2 engine. This strange improvization came about through the need to develop a towing aircraft large enough to be compatible with the Messerschmitt Me 321 Gigant troop glider. The He 111Z was evolved during 1941-42 and carried a crew of seven. Piloted from the port fuselage, it performed its task well, but its role disappeared when the Me 323 self powered version of the Gigant replaced the Me 321.

He.111Z

First flown in Spring 1941, two prototypes and 10 He 111Z-1 production aircraft were built.
For takeoff, 2 Jato rockets of 500 Kg were under each fuselage and 2 of 1500 kg under the central wing.

The adoption by the Spanish air force of those He 111Bs and Es which survived the civil war led, in 1941, to the Spanish government acquiring a licence to manufacture the later H 16 model at the CASA factory in Tablada, near Seville. Two hundred were ordered initially, but only 130 of these could be completed owing to the shortage in supply from Germany of the Jumo 211F engines to power them. Armed with a mixture of German and Italian guns (single MG 15s in the ventral gondola and in the rear of the crew cabin, and a 12.7 mm (0.5 in) Breda SAFAT in the nose blister) they were designated B.2H by the Spanish air force. These differed from the German built machines primarily in having a stepped crew compartment. Manufacturer’s designations divided them into C 2111A (bomber models), C¬2111C (reconnaissance bombers, with cameras in the starboard half of the bomb bay), and C 2111F (dual control bombing trainers). When the supply of Jumo engines ran out the eventual choice of a replacement fell upon the Rolls-¬Royce Merlin Mk 500 and 173 examples of this engine were purchased from Britain.

CASA 2111-D

These were used both to power additional CASA built aircraft (C 2111B bombers and C 2111D reconnaissance bombers, the latter having 1610 hp Merlins), and also to re-engine some of the earlier Jumo powered Heinkels. Spanish air force designation for all Merlin powered examples was B. 21; later, Jumo and Merlin powered bombers were included in 15 aircraft converted to T.8 (CASA C 2111E) nine passenger troop transports. The C 2111 series continued in Spanish air force service until the end of the 1960s.

CASA 2111

A total of around 7500 were built, including licence production in Romania and Spain (as the CASA 2111).
263 licence built Heinkel 111s were built by CASA as the 2111 as late as 1956.

Gallery

Engines: 2 x 1,200 hp Junkers Jurno 211 D.
Length: 54.6 ft. (16.63 m.)
Wing span: 74.1 ft. (22.6 m.)
Weight empty: 14,400 lb. (6,530 kg.)
Armament: 1 x 20 mm cannon 6 x 7.9 mm machine guns.
Max bomb load: 4,400 lb. (2,000 kg.)
Max speed: 267 m.p.h. (430 kph).
Range: 2,175 miles (3,500 km.).
Crew: 5

He 111B-2
Span: 22.6m (74ft 1.75 in)
Length: 17.5m (57 ft 5in).
Engine: 2 x Daimler-Benz DB 600CG, 708kW (950 hp)
Armament: 3 x 7.92-mm (0.312-in) mg, up to 1500 kg (3,307 lb) of bombs internally.
Max T/O weight: 10000 kg (22,046 lb).
Max speed: 230mph at 13,125 ft.
Operational range: 1,030 miles.
Crew: 4

He 111E
Engines: 2 x DB 601A, 1150 hp
Top speed: 254 mph
Range: 1100 mi at 215 mph
Armament: 6-8 mg / 1 x 20mm cannon

He 111E-A
Engines: 2 x Junkers Jumo 211D, 1200 hp
Top speed: 250 mph
Cruise: 212 mph
Range w/4000lb load: 760 mi
Max range: 2640 mi
Armament: 6-8 mg / 1 x 20mm cannon
Max bombload: 5600 lb

He 111 E 3
Span: 22.6 m (74 ft 13 in)
Length: 17.5 m (57 ft 5 in)
Maximum speed: 420 km/h (260 mph).
Height: 14 ft 7.25 in (4.4 m).
Engines: 2 x Junkers Jumo, 1000hp.
Max TO wt: 21,168 lb (9600 kg).

He 111H
Engines: 2 x DB 601A, 1150 hp
Top speed: 254 mph
Range: 1100 mi at 215 mph
Armament: 6-8 mg / 1 x 20mm cannon

He.111H-2
Engines: 2 x Junkers Jumo 211 F-2, 1340 hp.

He-111H-16
Engines: 2 x Jumo 211F-2, 1007kW
Wingspan: 22.60 m / 74 ft 2 in
Length: 16.40 m / 53 ft 10 in
Height: 4.00 m / 13 ft 1 in
Wing area: 86.50 sq.m / 931.08 sq ft
Max take-off weight: 14000 kg / 30865 lb
Empty weight: 8680 kg / 19136 lb
Maximum speed: 405 km/h (252 mph).
Ceiling: 6700 m / 22000 ft
Range: 1950 km / 1212 miles
Armament: 1 x 20mm cannon, 1 x 13mm machine-guns, 3 x 7.92mm machine-guns, 1000kg of bombs
Crew: 1

He 111 P 4
Span: 22.6 m (74 ft 11 in)
Length: 16.4 m (53 ft 91 in)
Gross weight: 13500 kg (29,760 lb)
Maximum speed: 320 km/h (200 mph).

He 111Z Twin Zwilling
Engines: 5 x Junkers Jumo 211F, 1350 hp
Propellers: three-bladed metal VDM variable
Wingspan: 35,20 m
Length: 16,60 m
Height: 4,20 m
Wingarea: 148 sq.m
Fuel capacity: 8250 lt
Empty weight: 21500 kg
MTOW: 28200 kg
Wing loading: 190,540 kg/sq.m
Power loading: 4,177 kg/hp
Max speed: 420 kph
Cruise speed: 375 kph
Climb rate:: 9000 m in 30 min
Ceiling: 9600 m
Range: 2400 km
Armament: 4 MT MG 131 of 13 mm, 2 x 2 MT MG 81Z 7,92 mm and 5 MG 81J 7,92 mm

CASA 2111D
Engine: 2 x RR Merlin 500, 1400 hp.
Wingspan: 74 ft 3 in
Wing area: 943 sq.ft
Length: 54 ft 6 in
Height: 13 ft 9 in
MTOW: 30,865 lb
Fuel capacity / wings: 760 gal
Fuel capacity / fuselage: 185 gal
Max speed: 260 mph
Cruising speed: 233 mph
Armament: 6 x 7.9 mm mg / 1 x 20 mm cannon
Bombload: 5510 lb

CASA 2111H-16-L
Wingspan: 74 ft 3 in
Length: 54 ft 6 in
Height: 13 ft 9 in
Empty weight: 17,000 lb
Loaded weight: 26,500 lb
Max speed: 250 mph at 17,000 ft
Service ceiling: 27,500 ft
Range w/max fuel: 1750 mi

Heinkel He 60

He 60D-1

The prototype He 60a (D 2325) first flew in 1933. It was designed by Reinhold Mewes, who had also been responsible for the He 59. The prototype was fitted with a 492kW / 660 hp BMW VI V type engine and a twin float undercarriage, and was used primarily for testing the floats. A second prototype, the He 60b, was powered by an uprated 750 hp engine, but this proved to be little more effective than the previous powerplant and the 660 hp version was reinstated in the third prototype and all subsequent production aircraft. The third prototype, the He 60c, was used for shipboard catapult launching trials and was the first post 1919 aircraft to be delivered to the German navy. In April 1933 the first of the initial pre-production batch of 21 He 60A machines was flown. They were to be used as land based trainers, but two were later modified with the addition of catapult equipment.
Still considered by the Heinkel company capable of carrying greater weights if given a more powerful engine, one He 60 was fitted with a 900 hp Daimler Benz DB 600, which increased the top speed by 45 km/h (28 mph), and was given the designation He 60B 3. Many trials were made with this aircraft but production never materialized. The main He 60C series were delivered to the German navy from late 1934 onwards. They were fitted with catapult hooks and armed with one movable 7.9 mm (0.311 in) MG 15 machine¬gun in the observer’s rear cockpit. Two were kept by Heinkel as test aircraft and eventually went to a training school. The D series which followed were fitted with improved radio and a forward firing 7.9 mm (0.311 in) MG 17 gun, but were later converted to unarmed trainers.
All production C and D series (totalling 200 aircraft) were built by the Arado and Weser companies. Following Heinkel practice the airframe was of steel tube and wood construction with fabric covering. Floats and engine cowling were of aluminium. A crew of two was carried in tandem open cockpits.
Before the Second World War, He 60s were deployed aboard every major warship of the German navy, but by 1939 had been replaced in the shipboard role by the Arado Ar 196. They were retained in shore based service in the North Sea, Baltic and Eastern Mediterranean until as late as 1943, and were eventually used for communication and training.

He-60
Engine: 2 x BMW VI 6.0 ZU, 485kW
Span: 12.9 m / 42ft 3.75 in
Length: 11.5 m / 37 ft 8.75 in
Max take-off weight: 3400 kg / 7496 lb
Empty weight: 2730 kg / 6019 lb
Max. speed: 225 km/h / 140 mph
Cruise speed: 215 km/h / 134 mph
Ceiling: 5000 m / 16400 ft
Range w/max.fuel: 900 km / 559 miles
Crew: 2
Armament: 1 x 7.92mm machine-guns

He 60

Heinkel He 59

He 59B-2

The design project for this large fuselage torpedo bomber/reconnaissance biplane was begun in 1930 by Reinhold Mewes of the Heinkel company, and was the largest of the company’s designs up to that time. The first prototype to fly, the He 59A (D 2215), was of sturdy appearance with a faired in wheeled undercarriage and was powered by two 492kW / 660 hp BMW VI liquid cooled engines. The airframe comprised a welded steel tube fuselage, with wooden frame wings, all of which were fabric covered.

Heinkel He 59 article

As its intended role was for overwater reconnaissance, all production models and the He 59B first prototype (which was the second example to fly) were fitted with twin float undercarriages. After service trials of the He 59A, production began in spring 1932 with a pre series batch of 16 armed He 59B-1s. It is fairly certain that these were built by Heinkel, but the next production orders, for 140 He 59B 2s and B 3s, were executed by the Arado Flugzeugwerke. The B series differed basically in internal equipment only. The B 1s were equipped with a 7.9 mm (0.311 in) ring mounted MG 15 machine gun in the extreme nose. Two additional MG 15s were fitted on the He 5913 2, in the dorsal and ventral positions. A crew of four was carried. A long range reconnaissance version, the He 59B 3, carried extra fuel in place of one of the guns.

In 1936 10 He 59B 2s were sent to Spain to join the Legion Condor, their floats prompting the nickname “Zapatones,” or “Big Shoes,” three of the planes being transferred to Franco when the Germans returned home.
The He 59C-1, used for training, had additional maritime navigation equipment installed and all armament deleted. The He 59C 2 was used for air sea rescue duties and it too was unarmed, carrying instead six dinghies plus additional radio equipment. Other variants included the He 59D 1 for air sea rescue and training, with a rounded, all metal ‘solid’ nose; the He 59E 1 torpedo trainer; and the He 59E 2 photographic reconnaissance trainer model. All of the C, D and E models were converted for their various roles from He 59B aircraft of the original order by the Walter Bachmann Flugzeugbau. The He 59N was a Bachmann conversion from the He 59D 1 for specialized navigation training duties, and was equipped to carry a practice torpedo plus smoke bombs.
Although more or less obsolescent when it entered service with the Luftwaffe in 1934, the He 59 was to remain in production for four more years and in service for about a decade, not disappearing finally from active duty until the middle of the Second World War. Its long service was due chiefly to the versatility of its roomy fuselage, virtually all of which was available for crew and payload since fuel was carried in the floats. In the maritime bomber role, this meant the ability to carry two 500 kg (1100 lb), four 250 kg (550 lb) or 12 50 kg (110 lb) bombs internally; or, alternatively, one or two 700 kg (1540 lb) or 1000 kg (2200 lb) externally slung torpedoes.
The He 59 was ‘blooded’ in the latter part of 1936 in the Spanish Civil War as part of the Luftwaffe’s Legion Kondor, operating both in the maritime role and as a night bomber. Some examples were fitted with a 20 mm (0.79 in) MG FF cannon for attacks on shipping. At the start of the Second World War there were still about 30 He 59s on the strength of the Kustenfliegergruppe (coastal aviation group) covering the North Sea area. In addition to the majority by then employed in various training roles, the He 59 continued in Luftwaffe service until as late as 1943 on air sea rescue, mine-laying, convoy-shadowing and coastal reconnaissance duties, latterly in the somewhat less dangerous waters of the Mediterranean, Aegean and Black Seas. It was important as an electronic-warfare platform and as a special trials aircraft.

Gallery

He 59B 2
Engine: 2 x BMW VI 6.0 ZU, 485kW
Max take-off weight: 9100 kg / 20,100 lb
Empty weight: 5440 kg / 11993 lb
Wingspan: 23.7 m / 77 ft 9 in
Length: 17.4 m / 57 ft 1 in
Height: 7.1 m / 23 ft 4 in
Wing area: 153.4 sq.m / 1651.18 sq ft
Max. speed: 240 km/h / 149 mph
Cruise speed: 205 km/h / 127 mph
Range w/max.fuel: 800 km / 497 miles
Crew: 4
Armament: 1-2 7.92mm machine-guns 15 or 1 x 20mm machine-guns FF cannon