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.
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.
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
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.
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.
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
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’.
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.
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
While work was proceeding with the P 1052 and the P1081, Hawker tried out the Snarler rocket on the P1040 which, with this addition, became the P1072. The Snarler was an Armstrong Siddeley rocket installation fitted to the tail of the aircraft, but powered by a Rolls-Royce Nene turbojet exhausting via bifurcated ducts in the wing roots, the idea being to get the rocket airborne for experimental engine development. After a conventional first flight in November 1950, the rocket was successfully used four days later. Six flights were made with the Snarler, taking off normally on the jet engine, and lighting the rocket at a fairly low altitude, putting the aircraft into a climb. With the Nene jet engine working at full power, together with the thrust of the rocket, the aircraft went up not beyond 40,000 feet the, aircraft had no pressurized cabin.
Engines: Rolls-Royce Nene turbojet, 5000 lb (2268 kg) and Armstrong Siddeley Snarler rocket, 2000 lb (907 kg) thrust.
The Harbin Songhuajiang-1 (松花江一号) was a Chinese unlicensed copy of the Aero Ae 45S produced in 1959.
Built at the Weijian State-owned Machinery Factory, Harbin, it first flew on 29 September 1959.
Engines: 2 x Walter Minor 4-III, 104 hp Propeller: two-blade Wingspan: 40ft 4,25in Length: 28ft 1,8in Maximum Take-off Weight: 3527 lb Crew: 1 + 5 Maximum Speed: 170.3 mph Range: 500.2 mi
In July 1982 it was reported that the Harbin Aircraft Works had developed a turbine-powered version of the Y-11, with PT6A-110 turboprops. A prototype was reputed to have flown. With a gross weight of 12,125 lb / 5500 kg, the maximum payload is 3748 lb / 1700 kg, and the Y-11T is estimated to have a max speed of 175 mph / 282 kph and a max range of 876 miles / 1410 km.
Developed from the earlier piston-engined Y-11, the twin-PT-6A-powered Y-12 has an enlarged cabin to accommodate up to 17 passengers. A first production batch of 18 aircraft was scheduled for completion by the end of 1986.
The Y-12 prototype first flew in 1982, and there have been three series production versions
Y12 (I) Initial version with 500 shp PT6A-11 engines, 93” diameter propellers, leading edge slats, seating for 17 passengers and a MTOW of 5000 kg.
Y12 (II) Later production version with higher-rated 600 shp PT6A-27 engines, plain leading edge, 98” diameter propellers and MTOW increased to 5300 kg. The UK CAA issued Type Certificate FA49 for this variant in 1990 and examples are in operation in Malaysia and Fiji.
Y12 (IV) Improved model with sweptback wingtips, redesigned seating for 18-19 passengers and max. weight increased to 5700 kg. The Canadian Aerospace Corporation markets a version of the aircraft under the Twin Panda name as a DHC-6 replacement.
The Sri Lankan Air Force ordered six Y-12 turboprop utility transports from China in 1986, and at least two have been delivered to the Chinese Air Force for aerial survey work.
The Y12 was originally produced by Harbin Aircraft Manufacturing Corporation (HAMC), and under Chinese commercial arrangements is marketed by the China Aviation Technology Import and Export Company (CATIC). HAMC has subsequently been reorganised in 1999 as Hafei Aviation Industry Co. Ltd (HAI), responsible for the Y12 and other sub-contract work.
Federal Aviation Administration Type Certificate: A00006WI applies to the Hafei Aviation Industry Company Limited Y12 IV.
Harbin Y 12 II Turbo Panda Engines: 2 x PT 6 A 27, 500 shp Length: 48.885 ft / 14.9 m Height: 18.373 ft / 5.6 m Wingspan: 56.43 ft / 17.2 m Wing area: 369.205 sq.ft / 34.3 sq.m Max take off weight: 11686.5 lb / 5300.0 kg Weight empty: 6262.2 lb / 2840.0 kg Max weight carried: 5424.3 lb / 2460.0 kg Max speed: 158 kt / 292 km/h Cruising speed: 135 kt / 250 km/h Initial climb rate: 1653.54 ft/min / 8.4 m/s Service ceiling: 22966 ft / 7000 m Wing loading: 31.78 lb/sq.ft / 155.0 kg/sq.m Range: 724 nm / 1340 km Crew: 2 Payload: 17pax
Y-12-II Engine: 2 x P&WAC PT6A. Installed pwr: 925 kW. Span: 17.2 m. Length: 14.9 m. Wing area: 34.3 sq.m. Empty wt: 2840 kg. MTOW: 5000 kg. Payload: 1700 kg. Cruise speed: 330 kph. Initial ROC: 528 m / min. Ceiling: 7000 m. T/O run: 180 m. Ldg run: 208 m. Fuel internal: 1600 lt. Range/payload: 1440 km with 800 kg. Capacity: 17 pax.
Y12 IV Engines: 2x Pratt & Whitney Canada PT6A-27 Propellers: 2x Hartzell HC-B3TN-3B/T10173(N)B-3 MCTOW 12,500 lb (5670 kg)
The Y-11 failed to attract export orders while equipped with Chinese radial engines, so it was converted to the Y-12.
In July 1982 it was reported that the Harbin Aircraft Works had developed a turbine-powered version of the Y-11, with PT6A-110 turboprops. A prototype was reputed to have flown. With a gross weight of 12,125 lb / 5500 kg, the maximum payload is 3748 lb / 1700 kg, and the Y-11T is estimated to have a max speed of 175 mph / 282 kph and a max range of 876 miles / 1410 km.
The H.230.01, service serial H.790, flew for the first time in June 1937. It was an advanced two-seat trainer which had a general resemblance to the H.220 but was of much lighter construction. Power was provided by two 127kW Salmson 6AF-00 engines and its configuration included a short crew canopy faired into the upper decking of the rear fuselage and a conventional . strut-braced tail unit, and the fixed main landing gear units incorporated spatted wheel fairings. During further tests it was decided to introduce considerable dihedral at the wingtips to improve stability, but the H.231.01 which followed in May 1938 had dihedral increased over the whole wing span, and the unusual wingtip arrangement of the modified H.230 was eliminated. Twin fins and rudders were introduced and power increased with 172kW Salmson 6AF engines. The Hanriot H.232.01 reverted to a single fin and rudder and had 164kW Renault 6 Q-o engines plus retractable landing gear. The H.232.02, first flown in August 1938, introduced a redesigned cockpit; it was tested officially between October 1938 and May 1939. The type was then given a twin fin and rudder tail assembly and was flown in this new configuration in December 1939, then redesignated H.232/2.01.
An order for 40 aircraft had already been received from the French air ministry, and this was increased to 57 examples shortly afterwards. By then known as the NC.232/2, they incorporated minor improvements including redesigned rudders and engine cowlings. Full navigational equipment was installed. Three reached Finland. Two were from Germany, and these were not taken into service until the Winter War 1939-40 with the Soviet Union was over. Deliveries to the Armee de I’Air started in February 1940, 35 being taken on charge up to the June 1940 Armistice. The NC.232/2s were,used by the training sections attached to the 51th and 54th Escadres, which were equipped with Breguet 691and 693 attack bombers. Twenty aircraft found on airfields when the German forces occupied Vichy, France, in 1942 were reduced to scrap.
Included among exhibits at the Salon de l’Aeronautique held in Paris in November 1936 was a striking all-metal twin-engined three-seat fighter. It had a somewhat abbreviated oval-section monocoque fuselage, a shoulder-mounted semi-cantilever wing carrying split trailing-edge flaps over its entire span and two 450hp Renault 12Roi 12-cylinder inline air-cooled engines projecting ahead of the fuselage nose. This, the H.220, had been designed to a C3 requirement prepared by the Service Technique de l’Aeronautique and issued in October 1934. Other contenders were the Breguet 690, the Potez 630, the Loire-Nieuport 20 and the Romano 110. As it became evident that the H.220 would be underpowered, the Renault engines were discarded in favour of 680hp Gnome-Rhone 14M 14-cylinder radials, and, with these installed, the first flight test was made at Avord on 21 September 1937.
The intended armament of the H.220 comprised two forward-firing 20mm cannon and two aft-firing 7.5mm MAC 1934 machine guns on a flexible mounting, but, in the event, no armament was fitted. On 17 February 1938, the prototype made a forced landing at Avord after losing the starboard propeller following a failure in the reduction gearbox. The poor stability evinced during flight testing of the H.220 (which had resulted in progressive changes in the contours and size of the vertical surfaces), coupled with inadequate internal capacity and some lack of sturdiness revealed by the forced landing (as a result of which the fuselage was irreparable), dictated major redesign, resulting in the H.220-2. After the partial destruction of the H.220, major redesign was initiated by the Societe Nationale de Constructions Aeronautiques du Centre, or SNCA du Centre, which had absorbed the Hanriot facility at Bourges on 1 February 1937. The oval-section monocoque fuselage of the original H.220 was discarded in favour of a fuselage built as two half shells mated by a central keel. An entirely new tail assembly with twin endplate vertical surfaces was fitted and the Gnome-Rhone 14M radial engines were enclosed by low-drag nacelles. These features were mated with the wing of the original H.220 to result in the H.220-2, which was first flown (as the H.220 No 02) on 17 March 1939. Four months later, in July 1939, this prototype was to be displayed statically as the NC 600 No 01 multi-seat fighter at the Salon de l’Aeronautique. In fact, the genuine NC 600 was to differ from the H.220-2 in several major respects.
H.220-2
H.220 Max take-off weight: 3700 kg / 8157 lb Empty weight: 2673 kg / 5893 lb Wingspan: 12.80 m / 41 ft 12 in Length: 7.87 m / 25 ft 10 in Height: 3.40 m / 11 ft 2 in Wing area: 21.16 sq.m / 227.76 sq ft Max. speed: 520 km/h / 323 mph Range: 850 km / 528 miles
H.220-2 Max take-off weight: 3850 kg / 8488 lb Empty weight: 2820 kg / 6217 lb Wingspan: 12.80 m / 41 ft 12 in Length: 7.87 m / 25 ft 10 in Height: 3.40 m / 11 ft 2 in Wing area: 21.16 sq.m / 227.76 sq ft Max. speed: 532 km/h / 331 mph Range: 770 km / 478 miles