Heinkel He 64

Two-seat sporting and training monoplane designed by twins Siegfried and Walter Gunter, and powered by a 112kW Argus As 8R inverted engine. Both cockpits were completely enclosed by a glazed coupe top. A small number were built.

He-64B
Engine: 1 x As-8a, 110kW
Max take-off weight: 780 kg / 1720 lb
Empty weight: 470 kg / 1036 lb
Wingspan: 9.8 m / 32 ft 2 in
Length: 8.3 m / 27 ft 3 in
Height: 2.1 m / 6 ft 11 in
Wing area: 14.4 sq.m / 155.00 sq ft
Max. speed: 245 km/h / 152 mph
Cruise speed: 222 km/h / 138 mph
Ceiling: 6000 m / 19700 ft
Range: 1500 km / 932 miles
Seats: 2

Heinkel He 58

He 58 D-1919 Bremen Atlantic being loaded onto the catapult on SS Europa

The concept was hit upon after Norddeutscher Lloyd (NDL) had carried a Junkers F.13 seaplane aboard the Lutzow during 1927 to provide joyrides for passengers when the liner was in port. NDL officials realised that a seaplane based on a liner could have a more practical commercial application, taking off with the liner’s airmail while still a long distance from port, therefore drastically cutting down time taken for the mail to arrive. Heinkel designed a catapult, which NDL planned to install on its new liners, the Bremen and Europa, and an aircraft to carry the mail. Since the crew of Lutzow had trouble providing the necessary maintenance for the F 13, Deutsche Luft Hansa agreed to provide the operational support for the venture, and when Bremen departed on her maiden voyage in 1929, a single HE 12 (D-1717) was carried aboard.

A second aircraft, (D-1919, Atlantik), was built for flying from Europa, sister-ship of the Bremen. Designated He 58, the second aircraft was slightly larger overall than the He 12, with increased payload and accommodation for the crew in a side-by-side open cockpit. Power was supplied by a 370 kW (500 hp) BMW Hornet A, initially un-cowled, but later fitted with a full long-chord cowling with cooling slits in the forward face.

The He 58, (D-1919, Atlantik), continued in service on Europa until replaced by Junkers Ju 46 floatplanes.

He 58
Engine: 70 kW (500 hp) BMW Hornet A
Wingspan: 17.2022 m (56 ft 5.25 in)
Wing area: 49.4 m2 (532 sq ft)
Length: 11.7793 m (38 ft 7.75 in)
Height: 4.70 m (15 ft 5 in)
Empty weight: 1,850 kg (4,078 lb)
Gross weight: 3,140 kg (6,922 lb)
Payload: 200 kg (440 lb) of mail
Maximum speed: 204 km/h (127 mph)
Cruise speed: 159 km/h (99 mph)
Service ceiling: 3,800 m (12,500 ft)
Crew: Two, pilot and radio operator

Heinkel He 46

During the early 1930s, the German military was beginning to build up in strength – the RLM (German Air Ministry) wanted aircraft that could be rapidly built and would be able to swell the Luftwaffe’s inventory with large numbers of aircraft for training. Ernst Heinkel designed many of these early aircraft, with the He 46 being created to fill this short-range reconnaissance and army co-operation role for the Luftwaffe.

The prototype flew for the first time toward the end of 1931. Although following the general Heinkel biplane configuration it did have an abnormally large upper wing with marked sweepback and a very small lower wing. It was otherwise a conventional biplane, with a mixed construction consisting of metal framework and fabric covering, and a slightly swept back (10°) upper wing, powered by a 450hp Siemens-built Bristol Jupiter radial engine. The tailplane was mounted high and braced by struts. The undercarriage was fixed, and the tail was fitted with a skid rather than a wheel. The observer’s view of the ground was considerably restricted and the aircraft was subsequently altered to a parasol monoplane design by removing the lower wing and increasing the span of the upper by 2.5 m (8 ft 2.5 in) and braced to the fuselage with strut-braces: the second prototype, the He 46B was built to this design (overall the upper wing area was increased by 22%). Both machines were initially powered by the Siemens built 450 hp Bristol Jupiter engine, but trials proved that this had insufficient capacity and in 1932 the 650 hp Siemens SAM 22B nine cylinder radial was installed. This was considered satisfactory during trials on the third (and first preproduction) aircraft, the He 45C, which was equipped with radio and fitted with a 7.9 mm (0.311 in) MG 15 machine gun in the observer’s rear cockpit. The He46b first flew in early 1932.

By 1934, the He 46C had been ordered in sufficiently large numbers to improve the now rapidly expanding Luftwaffe. Production began with the He 46C-1 in 1933. This was similar to the 46c, but with the ability to carry either a camera or 440lb of small bombs under the rear cockpit. The He 46C-1, similar to the He 46C but having a bay beneath the observer’s cockpit to carry photographic equipment or up to 20 10 kg (22 lb) bombs.

Heinkel’s order book for 1933 included 478 of these aircraft, including exports to Hungary and Bulgaria, and in order to fulfil these obligations licence production was undertaken by Siebel Flugzeugwerke (159 C 1s), MIAG (83 C, E and F series), Gothaer Waggonfabrik at Gotha (24 CA/C 2s), and the Fieseler Flug-zeugwerke (12 C Is). Two hundred (194 of which were C 1s) were built at Heinkel’s Warnernfinde factory, in addition to the three prototypes.

A prototype conversion of the He 46C-1 in 1934 was made for the D series, with only minor improvements over its predecessors. This was followed by six pre-production C-1 conversions to the He 46D-0s, with a number of minor changes. One D 1, fitted with the NACA engine cowling and designated He 46e, became the prototype for the E series. Built for the Luftwaffe in E 1, 2 and 3 variants, they differed slightly in equipment installations, but the 2 was the only one to be fitted with an engine cowling that increased maximum speed by 16mph but that made maintenance rather more difficult and was often removed. An He 46C fitted with a 560 hp Armstrong Siddeley Panther cowled engine became the prototype (He 46f) for a new unarmed observer trainer series F 1 and 2 (14 built).

The original total of 478 ordered had been completed by 1936 when production ceased, but a few continued into Second World War service, until eventually replaced in the short range reconnaissance role by Henschel Hs 126s. Some of those remaining during the war were in service with Nachtschlachtgruppen (night attack groups) on the Russian Front, along with their Hungarian counterparts.

By the time production finished in 1936 the He 46 was the main equipment of the Luftwaffe’s Auflärungsstaffeln (H), but early in 1938, at the time of the Ilmavoimat’s evaluation, it had begun to be replaced by the Henschel Hs 126A-1. As such, the aircraft was cheap and readily available and there had already been export sales to Bulgaria and Hungary (eighteen He 46C-2s (C-1s but with engine cowling) were sold to Bulgaria, while Hungary purchased a number of He 47E-2s.

The Bulgarian batch of 18 aircraft were designated He 46C¬2, and fitted with a NACA engine cowling, which increased the maximum speed by 26 km/h (16 mph). Hungarian aircraft were designated He 46E 2, and gave useful service as late as 1942 43, in bombing operations and as attack aircraft against the USSR. In Sep¬tember 1936, during the civil war, 20 He 46C¬1s had also been sent to Spain.

At the time the Ilmavoimat / Maavoimat evaluation team looked at the He 46, it was already largely phased out of front-line service with the Luftwaffe. The aircraft were offered for sale “as is” at an attractive per-unit cost far below any of the newer aircraft on the market and available. Serious consideration was in fact given to this offer, particularly as delivery was immediate.

A few were still in use in September 1939 two units were still equipped with the He 46 at this stage), and saw service in Poland. By the time Germany invaded France in 1940, all He 46 aircraft had been withdrawn from operational service, although they did continue service in training units. A final period of front-line service came in 1943, when a shortage of more suitable aircraft meant that the Luftwaffe was forced to take the aircraft from the training units and used a number of He 46s on night harassment missions on the Eastern Front. The He 46 saw service in Spain, twenty He 46C-1s given to the Spanish Nationalists in September 1938. The Hungarian aircraft took part in the invasion of the Soviet Union in 1941, equipping the 1st Short-Range Reconnaissance Squadron, and with the 3/2 Short-Range Reconnaissance Squadron in 1942. The Hungarian aircraft were also used as bombers, before being replaced with the Focke-Wulfe 189 during 1943.

He-46C
Engine: 1 x Bramo SAM 322, 480kW
Max take-off weight: 2300 kg / 5071 lb
Empty weight: 1765 kg / 3891 lb
Wingspan: 14.0 m / 45 ft 11 in
Length: 9.5 m / 31 ft 2 in
Height: 3.4 m / 11 ft 2 in
Wing area: 32.2 sq.m / 346.60 sq ft
Max. speed: 260 km/h / 162 mph
Cruise speed: 220 km/h / 137 mph
Ceiling: 6000 m / 19700 ft
Range w/max.fuel: 1000 km / 621 miles
Armament: 1 x 7.9mm machine-guns
Crew: 2

He 46C-1
Engine: amo 322B (SAM 22B), 485kW (650 hp).
Span: 14m (45ft 11.25 in)
Length: 9.5m (3l ft 2in).
Max T/O weight: 2300 kg (5,071 lb)
Max speed: 161 mph at 2,625 ft.
Operational range: 615 miles.
Armament: 1 x 7.92-mm (0.312-in) mg, up to 200 kg (440 lb) external

He 46D

He 46E

He 46F
Engine: Armstrong Siddeley Panther, 418-kW (560-hp)

Heinkel He 12

The Heinkel HE 12 was a pontoon-equipped mail plane built in Germany in 1929, designed to be launched by catapult from a liner at sea.

The concept was hit upon after Norddeutscher Lloyd (NDL) had carried a Junkers F.13 seaplane aboard the Lutzow during 1927 to provide joyrides for passengers when the liner was in port. NDL officials realised that a seaplane based on a liner could have a more practical commercial application, taking off with the liner’s airmail while still a long distance from port, therefore drastically cutting down time taken for the mail to arrive. Heinkel designed a catapult, which NDL planned to install on its new liners, the Bremen and Europa, and an aircraft to carry the mail. Since the crew of Lutzow had trouble providing the necessary maintenance for the F 13, Deutsche Luft Hansa agreed to provide the operational support for the venture, and when Bremen departed on her maiden voyage in 1929, a single HE 12 (D-1717) was carried aboard.

With the catapult the aircraft took-off at 110 kph / 69 mph at the nd of a ramp 20 m / 65 ft long.

The HE 12 was a derivative of the military HE 9 design; a conventional, low-wing, strut-braced monoplane. The pilot and radio operator sat in tandem, open cockpits with the mail carried in a compartment behind them.

On 22 July, while still 400 km (250 mi) out of New York City, Bremen successfully launched the HE 12. When the seaplane was unloaded 2+1⁄2 hours later, mail from Berlin had taken just 6+1⁄2 days to reach New York. The next day, in front of a crowd of 3,500 people, mayor Jimmy Walker christened the HE 12 with the name of the city. On the return journey, the newly christened New York launched from Bremen near Cherbourg on 1 August, landing in Bremerhaven four hours later, in time for the mail to be transferred to another aircraft and arrive in Berlin the same afternoon, 5+1⁄2 days after leaving New York. Use of the seaplane saved around 20 hours on the westward trip, and 1–2 days on the eastward journey.

HE 12 (D-1717, New York) flew regularly from Bremen until severely damaged in an accident at Cobequid Bay on 5 October 1931.

Engine: Pratt & Whitney Hornet, 450 hp
Wingspan: 16.7958 m (55 ft 1.25 in)
Wing area: 48.46 sq.m (522 sq ft)
Length: 11.56 m
Height: 4.60 m (15 ft 1 in)
Empty weight: 1580 kg (3,483 lb)
Normal take-off weight: 2600 kg (5,732 lb)
Payload: 200 kg mail
Maximum speed: 216 km/h
Cruise: 192 km/h (119 mph, 103 kn)
Range: 1600 km
Service ceiling: 3,800 m (12,500 ft)
Crew: 2

Heinkel He 8

The He 8 floatplane, a development from the He 4 and 5, appeared in the autumn of 1927.

A single-engined seaplane with three seats inline in separated open cockpits. A low wing monoplane, braced underwing with by 4 pairs of masts in N configuration uniting the two floats in the catamaran and the base of the fuselage. The cantilever horizontal stabilizer was on the back of the fuselage. Construction was wood and fabric for the aerofoil, wood and plywood for the fuselage.
Powered was a 335kW / 450 hp Armstrong Siddeley Jaguar radial engine.
Twenty two were ordered by the Danish naval flying corps, 16 of which were built in Denmark under the designation H.M.II. They were mainly used for reconnaissance and survey work as far north as Greenland. Some served until 1940. Maximum level speed was 218km/h. Armament comprised a rear-mounted machine-gun.
Total production: 22

Engine Armstrong Jaguar IV 420 hp
Propeller: two-bladed wooden fixed pitch
Wingspan: 16,80 m / 55 ft 1.5 in
Length: 11,50 m / 37 ft 8.3 in
Height: 3,90 m
Wing area: 49 sq.m
Empty weight: 1500 kg
MTOW: 2325 kg / 5126 1b
Wingg loading: 47,5 kg.sq.m
Power loading: 5,476 kg/hp
Max speed: 210 kph
Ceiling: 6000 m
Range: 800 km
Armament: 1 Madsen 7,7 mm

Heinkel He 7

The He 14 biplane designed as a torpedo carrier in 1925 had proved unsuccessful, for the lack of a suit-able powerplant, but in 1927 a three seat monoplane development appeared as the He 7. Powered by a 450 hp Bristol Jupiter VI engine, it showed more promise than its precursor. Production He 7s had three sep¬arate cockpits.

Heinkel He 6

By 1927 the German authorities were becoming less intimidated by the restrictions imposed by the Versailles Treaty, and in that year Heinkel produced the He 6 reconnaissance seaplane. This incorporated much navigational and wireless equipment obviously with a view to future military use. The He 6 was a three/four seat long range monoplane, with an enclosed cockpit for the pilot, navigator and radio operator. Powerplant was an 800¬hp Packard engine.

Heinkel He 5

Development of the basic design continued with the He 4 and He 5 reconnaissance seaplanes produced in 1926. Production figures for the He 5 are also unknown. It was fitted with the 335kW / 450 hp Napier Lion engine, and proved itself by gaining three world seaplane climb/payload records in September 1926.

A single-engined float seaplane, with three seats inline in separated open cockpits. A monoplane low wing braced underneath by 4 pairs of masts in N configuration uniting the two floats in the catamaran and the base of the fuselage. The cantilever horizontal stabilizer was directly on the back of the fuselage, two floats in catamaran. The He5 was constructed of wood, with a plywood wood coating for the fuselage.

The He 5 was licence-built in Sweden for the Navy by Svenska.

In the second-half of the 20’s the Soviets decided to acquire an aircraft carrier. Realising that experience of design of catapults nor suitable aircraft was in the country, thel VVS turned to the German firm “Ernst Heinkel.
In 1927 the Soviets purchased two He.5 float monoplanes. Tests showed that the flight-performance data was considerably lower than declared by firm, but the aircraft was steady, and it possesses not bad maneuverability. These machines served for a while in 65- m squadron, which was in Nakhimova bay in Sevastopol.
Total production: 100

He 5
Engine Napier Lion II, 450 hp
Propeller two-bladed wooden fixed pitch
Wingspan: 16,80 m
Length: 12,19 m
Height: 4,23 m
Wung area: 49 sq.m
Empty weight: 1634 kg
MTOW: 2900 kg
Wing loading: 59 kg/sq.m
Power loading: 6,4 kg/hp
Max speed: 230 kmh
Ceiling: 6000 m
Range: 800 km
Armament: 2 x 7,92 mm mg

He 5b
Engine: Bristol-board Jupiter VIII, 480 hp

He 5c
Engine: Bristol Pegasus IIm3, 660 hp
Max speed: 280 kph
Ceiling: 7000 m

Heinkel He 4

Development of the basic design continued with the three-seat He 4 and He 5 reconnaissance seaplanes produced in 1926.
A single-engined three-seater with inline separated open cockpits. A monoplane low aerofoil braced under-wing by 4 pairs of masts in N configuration, uniting the two floats in the catamaran and the base of the fuselage. The cantilever horizontal stabilizer was placed directly on the back of the fuselage. Construction wood and fabric covered aerofoil, wood and plywood coating for the fuselage.
The He 4 was powered by the 268kW / 360-hp Rolls Royce Eagle IX, but it is doubtful whether it was produced in large numbers.
The He 4 was licence-built in Sweden for the Navy by Svenska.

Engine Rolls-Royce Eagle IX, 360 hp
Prop two-bladed wooden fixed Pitch
Wingspan: 17,99 m / 59 ft
Length: 12,50 m / 41 ft
Height: 3,65 m
Wing area: 52,50 sq.m
Empty weight: 1761 kg
MTOW: 2500 kg / 5510 1b
Wing loading: 47,619 kg/sq.m
Power loading: 6,944 kg/hp
Max speed: 180 kmh / 112 mph
ROC: 222 m/min
Landing speed: 87 km/h
Ceiling: 3800 m
Range: 800 km.

Heinkel He 3

The He 3 which followed later in 1923 was a small cantilever monoplane with a monocoque wooden fuselage, accommodation for a crew of three, and powered by a 75 hp Siemens Halske radial. Its most interesting features were the easily removable wings and an undercarriage which allowed the quick interchange of landing wheels and floats. It is not known how many He 3s were built, but the type was used mostly for exhibition and sporting purposes. One, with a 100 hp Siemens engine, was first in its class at the 1923 Gothenburg seaplane exhibition.