Category Archives: Luftwaffe

Deutschland / Germany

Fighterbomber, Projects

Messerschmitt Zerstörer-Projekt, Ausführung II, (Destroyer-project, Scheme II), (Unicraft Models, Resin)

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TYPE: Destroyer, ground-attack aircraft

ACCOMMODATION: Pilot only

POWER PLANT: One turbojet-engine, type unknown

PERFORMANCE: No data available

COMMENT: After the end of “WW II, when the Allied occupied Germany they found a huge amount of secret project documents. Among these were several unconventional designs from the Messerschmitt Company e. g. the so called “Animal Names” types. These were a single-turbojet  midget fighter “Libelle”  (Dragonfly) and two designs of the “Wespe I” and „Wespe II“ (Wasp) light fighters, a twin-engine fighter“ Me P.1079/18 „Schwalbe“(Swallow),  a bomber-transporter “Wildgans” (Brant) and two versions of a heavy ground-attacker “Zerstörer –  Projekt I” and „Zerstörer – Projekt II“ (Destroyer I and II).
As far as these latter are concerned these projects appear to consist of studies from the period 1941/42. But very unusual for Messerschmitt project drawings is that none of the dotted-outline turbojets matched  with the contures of any turbojets that were under development by BMW, Daimler-Benz, Heinkel-Hirth, Junkers and Porsche nor do the thrust figures quoted for them correpond to the known turbojet variants in production or development at that time.
An other confusing fact is that the Zerstörer ProjektII had the air intakes in the wing rootes and the sole turbojet engine was located in the rear fuselage. But additionally there were two openings on both sides the fuselage and the wings leading edges. This could be interpreted that the Zerstörer project II was powered by two turbojet engines.
On the other hand the high T-tailplane leads to the assumption of a later design period 1944/45. Focke-Wulf employed the T-taiplane for the first time in 1945 in the design of the Tank Ta 183. Messerschmitt, Heinkel and other aircraft manufacturers followed hastingly, as too little was known of the related flying characteristics of this type of tail surface. After the war the Allied quickly recognized its advantage and adopted this design feature.
Finally, a further factor indicating that the Zerstörer-designes were of later vintage is that both designes had a nosewheel tricycle undercarriage – a design feature that was first introduced in the Messerschmitt Me 262. Also, the rearward reclining seat and flush canopy blending into the fuselage nose contures  were not features of high-speed aircraft designes oft he 1941/42 period.
In conclusion and perhaps more likely is the fact that these designs are more after war fantasy than reality. So this comment is in contrast to the comment, given with the Messerschmitt Zerstörer-Projekt, Ausführung I, (Destroyer-project, Scheme I) on that website.

(Ref.: Herwig, Dieter and Heinz Rode: Luftwaffe Secret Projects, Ground Attack & Special Purpose Aircraft. Midland Publishing, Hinckley, LE10 3EY, England)

Fighter, Projects

Messerschmitt “Projekt Wespe I” (Project Wasp I), (Unicraft Models, Resin)

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TYPE: Short-range fighter, interseptor

ACCOMMODATION: Pilot only

POWER PLANT: One turbojet engine of unknown type

PERFORMANCE: No data available

COMMENT: The end of WW II saw a great amount of  secret project documents burned, captured or left to blow around empty hangars. Some companies documents were almost completely lost, others were scattered. After the war some of these seemingly reappeared but most likely many of these projects are imaginations. Some were relatively conventional, others were futuristic, but it is unknown whether these designs are from the period 1940/41 or from the time at the end of the WW II.
This is true for instance for Messerschmitt’s “Animal Names” types. These were a single-turbojet  midget fighter “Libelle”  (Dragonfly) and two designs of the “Wespe I” and “Wespe II” (Wasp) light fighters, a twin-engine fighter Messerschmitt Schwalbe (Swallow),  a bomber-transporter “Wildgans” (Brant) and two versions of a heavy ground-attacker “Zerstörer I” and “Zerstörer II” (Destroyer).
Both Messerschmitt “Wespe I” and “Wespe II” had swept-back wings, were to be powered by a single turbojet-engine and had a tricycle landing-gear. From this point of view these projects could be dated to the end of the war.
In contrary, unusual for these Messerschmitt project drawings is that none of the dotted-outline turbojets in each of the drawings matches with the contours of any turbojets that are under development or production by BMW, Daimler-Benz, Heinkel-Hirth and Junkers, nor do the thrust figures quoted for them correspond to the known turbojets variants. Gas turbine development in Germany was concerned from the very beginning with the axial-flow type, save for the radial-flow turbojets developed by Dr. ing. von Ohain. This leads to the conclusion that at beginning of the war Messerschmitt possessed no documentation on turbojet development or installation plans hypothesizing that all these “Animal Name” projects could also be dated to the early 1940’s.
In conclusion, perhaps and more likely are these designs the product more of fantasy than reality.

(Ref.: Herwig, Dieter and Heinz Rode: Luftwaffe Secret Projects, Ground Attack & Special Purpose Aircraft. Midland Publishing, Hinckley, LE10 3EY, England)

Nightfighter

Heinkel He 219B-1”Uhu” (Eagle-Owl), III./NJG3, (Dragon Models)

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TYPE: Night Fighter

ACCOMMODATION: Crew of three

POWER PLANT: Two Junkers Ju 222 liquid-cooled radial engines, rated at 2,500 hp each, resp. two Daimler-Benz DB 603 liquid-cooled engines, rated at 1,900 hp each

PERFORMANCE: 435 mph

COMMENT: The Heinkel He 219 „Uhu“ (Eagle-Owl) was a night-fighter that served with the German Luftwaffe in the later stages of World War II. A relatively sophisticated design, the He 219 possessed a variety of innovations, including Lichtenstein SN-2 advanced VHF-band intercept radar, also used on the Junkers Ju 88G and the Messerschmitt Bf 110G night fighters. It was also the first operational military aircraft to be equipped with ejection seats and the first operational German World War II-era aircraft with tricycle landing gear. Had the „Uhu“ been available in quantity, it might have had a significant effect on the strategic night bombing offensive of the Royal Air Force; however, only 294 of all models were built by the end of the war and these saw only limited service
By the end of 1944, the Luftwaffe had accepted 214 Heinkel He 219As, but during the previous November, the promulgation oft he „Jäger-Notprogramm“ (Fighter Emergency Programme) had sounded death knell for all twin piston-engine fighters with the sole exception of the Dornier Do 335 Pfeil. Ernst Heinkel tacitly ignoring the RLM edict and finalized an assembly line for the fighter at Oranienburg.
Prior to the creation of the „Jäger-Notprogramm“ several variants of the basic He 219 had reached advanced development and even initial production stages. The follow-on series to the He 219As in service was to be the He 219B fitted with the new, but troublesome 2,500 hp Junkers Jumo 222A/B 24 cylinder engines – a multibank, liquid-cooled inline engine, with six rows of cylinder blocks having four cylinders each—which would have allowed the He 219 to reach 440 mph, each of which were almost the same displacement in their A/B (supercharged) and E/F (supercharged with intercoolers) versions and each only very slightly heavier, compared to the Pratt & Whitney R-2800 Double Wasp radial engines in the American Northrop P-61 „Black Widow“ night fighter. The He 219B wing was also to have had an increased span of 22.06 m for better high altitude performance. The Jumo 222 did not reach production status, with just under 300 examples built in at least three differing displacement sizes. Only a few test machines were ever fitted for the engines; some additional air frames were built with the enlarged wing. These examples were slated to fly with high-altitude versions of the standard DB 603 powerplants in place of the troubled Jumo 222 multibank powerplants, but only one or two test machines ever flew with them.
It was proposed to install the Junkers Jumo 222 in a high-altitude three-seat model, the Heinkel He 219B-1, but the non-availability of the Junkers engine necessitated the installation of the Daimler-Benz DB 603Aa in a sole exemple of this variant completed and tested. This He 291B-1 had an aerodynamically refined cockpit canopy, a lengthened fuselage, and an extended wing spanning. Flight testing was cut short when, during the second landing, the starboard undercarriage leg collapsed and the aircraft suffered such intensive damage that it had to be scrapped.
The second B-series, the Heinkel He 219B-2, was intended specifically for anti-Mosquito operations, and was similar in concept of the He 219A-6 in being stripped of virtually all armor.  Employing an He 219A-5 two-seat fuselage married to a long-span B-series wings it was powered by Daimler-Benz DB 603 engines with TK 13 turbo-superchargers, but only few additionally aircraft of this type were hurriedly completed. These were placed in operational service with a forward-firing armament of two 20-mm MG 151 cannon in the wing roots, and  two 30-mm MK 108 cannon  in a „Schräge Musik“ installation.
The Heinkel He 219B-3 was similar to its predecessor apart from the reinstatement of ventral tray armament comprising two 30-mm MK 108 and two 20-mm MG 151 cannon, and this, too, was to have been powered by two Daimler-Benz DB 603L engines, but while still under construction, Heinke received  a directive from the Technischen Amt to await delivery oft he Junkers Jumo 222 engines for installation in this aircraft. In the event, the Junkers power plants never arrived and, in consequence, the He 218B-3 never left the ground (Ref.: 8).

Fighter, Projects

Messerschmitt Me P. 1106/II (RS-Models, Resin)

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TYPE: Fighter, Interceptor, Project

ACCOMMODATION: Pilot only

POWER PLANT: One Heinkel-Hirth HeS 011 turbojet engine, rated at 1.300 kp thrust

PERFORMANCE: No data available

COMMENT: The Messerschmitt Me P.1106 was a proposed German fighter aircraft project near the end of WW II. It was intended as an improvement to the Messerschmitt Me P. 1101.
On December 15, 1944 Messerschmitt design team decided to submit another design alongside the Me P.1101 – the Messerschmitt Me P. 1106. This was an advanced update on the final version of the Me P.1092/5 which had been drafted in July 1943 but also bore some similarities to the Me P.1101.
The Messerschmitt Me P. 1106 was redesigned several times. It had a nose air intake and fuselage mounted turbojet-engine. The wings of each design were swept back at 40 degrees. The planned powerplant was a Heinkel-Hirth HeS 011 turbojet engine, and armament was to be two 30 mm MK 108 cannons
The first version (Me P. 1106/I) had a short fuselage and a T-tail with the cockpit faired into the vertical stabilizer, similar to the Lippisch Li P.13a.
The redesigned version shown here  (Me P. 1106/II), had a very short fuselage, too, the vertical stabilizer was changed to a tail plane of butterfly style and the cockpit was housed far aft. This odd shape apparently gave the best aerodynamic performance Messerschmitt and his team had yet achieved but the disadvantage was a poor visibility for the pilot.
A third and final design (Me P. 1106/III) had a longer and slim fuselage with a V-tail plane and the cockpit moved slightly forward.
All projects of the Messerschmitt Me P. 1106 were abandoned since the performance of the Me P.1101 had not been improved on (Ref.: 17, 22, 24).

Fighter, Projects

Blohm & Voss Bv P.202 (Unicraft Models, Resin)

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TYPE: Variable-wing fighter. Project

ACCOMMODATION: Pilot only

POWER PLANT: Two BMW 003 turbojet engines, rated at 850 kp each

PERFORMANCE: No data available

COMMENT: The Blohm & Voss P 202 was an unusual design study for a variable-geometry turbojet fighter during World War II. It was the first design to incorporate a slewed wing (also known as an oblique or scissor wing) in which one side swept forward and the other back.
During WW II in Germany intensive work has been done in concern of influence back-swept wings on high-speed aircraft. Calculations as well as wind-tunnel tests showed that swept wings could minimize the effects of compressibility as the speed of sound was approached. But sweeping the wings causes problems of its own, especially at the low speeds used for takeoff and landing. A variable-sweep mechanism was one possible solution but it would be complex, heavy and expensive. It also has problems with movement of the centre of lift. Both backwards and forwards sweep were investigated and they proved to have opposite disadvantages. Sweeping one wing forwards and the other back would balance out the aerodynamic problems and a one-piece slewed wing approach would not need such a complex sweep mechanism.
In 1944, with their project Bv P.202 the design team of Blohm & Voss tried to compensate the disadvantage of swept-back wings a low speed by turning a single full-span wing in its yaw axis so that one side sweeps back and the other side sweeps forward. The shoulder mounted wing was shaped as a disc in the mid-wing section. During take-off and landing as well as at lower speed the wing was in rectangular position with all buoyancy forces such as airbrakes and spoilers still effective. At high speeds the whole wing was slewed at 35° that the left wing showed forward and the right wing backward. The wing span was 39.4 ft when unswept and 32.8 ft when fully swept. Because the fuselage was filled with wing-rotation machinery, the landing gear extended down from the wing main spar, and was very long, while the nose gear retracted backwards into the fuselage. The Blohm & Voss Bv P.202 was powered by a pair of BMW 003 turbojets, slung underneath the fuselage center section and exhausting behind the wing. Provision for three forward-firing cannon was made in the nose. Due to the war situation in Germany the project never left the drawing board (Ref.: 18, 24).

Nightfighter

Messerschmitt Me 262 with Heinkel/Hirth HeS 011A, (Frank/Airmodel, Vacu-formed, with parts from Revell)

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TYPE: Night and bad-weather fighter

ACCOMMODATION: Crew of two, pilot and navigator/radar-operator

POWER PLANT: Two Heinkel/Hirth HeS 011A turbojet engines, rates at 1.300 kp thrust each

PERFORMANCE: 540 mph at 19,685 ft

COMMENT: The Messerschmitt Me 262, nicknamed Schwalbe (German: “Swallow”) in fighter versions, or Sturmvogel (German: “Storm Bird”) in fighter-bomber versions, was the world’s first operational turbojet-powered fighter aircraft. Design work started before WW II began, but problems with engines, metallurgy and top-level interference kept the aircraft from operational status with the German Luftwaffe until mid-1944. The Me 262 was faster and more heavily armed than any Allied fighter, including the British turbojet-powered Gloster Meteor. One of the most advanced aviation designs in operational use during World War II, the Me 262’s roles included light bomber, reconnaissance and experimenat night fighter versions.
While the Messerschmitt Me 262 was not a difficult aircraft to fly, it possessed its share of idiosyncrasies, and some problems arose in the conversion of inexperienced pilots who had just completed their fighter training on piston-engined types. So it was obvious that traing would be simplified by the availability of a dual-control two-seater, and, accordingly, Messerschmitt evolved a suitable conversion trainer, the Messerschmitt Me 262B-1a.
Only some 15 examples of this trainer were delivered as the importance  attached to the introduction of the Me 262 as a nocturnal interceptor resulted in additional trainers on the assemblxy line being converted  as night fighters under the designation Messerschmitt Me 262B-1a/U1.
Whereas the Me 2626B-1a/U1 was a hurried adaption of the training model, the Messerschmitt Me 262 with two more powerful Heinkel/Hirth HeS 011A turbojet engines was considered as the definitive night-fighting sub-type for service from mid-1945. Structurally, the principal change consisted of the insertion of additional fuselage section fore and aft the tandem cockpits, increasing overall length more than 3.5 ft. This provided the necessary space to restore the 900 ltr resp. 600 ltr fuel tanks.
The first aircraft possessed similar radar to that of the Me 262B-1a/U2, and flight trials should begin in March 1945. The drag of the „Hirschgeweih“ array, with its eight 7-mm-diameter dipoles, was such that it reduced maximum speed by 30 mph. Various attempts had been made to streamline the antennae, resulting in the „Morgenstern“ aerial system in which the short antennae protruded through the pointed nose cone, and it was calculated that this would restore 30 mph of the speed loss. In the event, it was decided to standardize on the centrimetric wavelength FuG 240 „Berlin“ radar with a disc scanner housed in a plastic radome above the nose-mounted cannon, this affording little or no drag. The second variant of this design was to be fitted with two Heinkel/Hirth HeS 011B turbojet engines of 1.500 kp thrust each, equipped with a „Berlin“ radar, and a crew of three in a pressurized cockpit.  The Me 262 night fighter variants retained the standard forward firing battery of four 30 mm MK 108 cannon, and, in addition, provision was made for two similar weapons in a „Schräge Musik“ arrangement immediately aft of the rear cockpit (Ref.: 7).

Fighterbomber, Medium Bomber, Projects

Messerschmitt Me P.1101/28 (Resin, Frank Modellbau)

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TYPE: Fast bomber and destroyer

ACCOMMODATION: Crew of two (Pilot and radiooperator/navigator)

POWER PLANT: Two Heinkel-Hirth HeS 011 turbojet engines, rated at 1.300 kp thrust each

PERFORMANCE: 565 mph

COMMENT: This project study of 11. April 1945 (Little note: less than four weeks before the total collaps of the “Third Reich”!!!!) for a two seat “Schnellbomber” (fast bomber) and “Zerstörer” (destroyer) constituted a further development of the Messerschmitt Me P.1099, Me P.1100 and Me P.1101 series of proposals of 1944 on the basis of the original in service Messerschmitt Me 262.
Whereas the basic fuselage, spacious cockpit and tail surfaces of the mentioned follow-up proposals were retained, the two Heinkel-Hirth HeS 011 turbojets were relocated into the wing root to which the new wings having a leading edge sweep of almost 40 degrees were attached. An interesting feature of the design was that the mainwheels were to retract inwards to rest vertically in the fuselage between the fore and aft fuel tanks. Exactly how this was to be accomplished with the turbojets in the way is not clear from the documents. Although the final form of the fuselage nose portion had not been decided, the end of the war brought an early end of the project (Ref.: 16).

Fighter

Messerschmitt Me 263 “Scholle” (Plaice), (Huma)

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TYPE: Fighter interceptor

ACCOMMODATION: Pilot only

POWER PLANT: One Walter HWK 109-509C-3 dual-chamber liquid-propellant rocket engine,main chamber rated up to 2,000 kp thrust, auxiliary chamber 400 kp thrust

PERFORMANCE: 590 mph

COMMENT: The Messerschmitt Me 263 „Scholle“ (Plaice) was a rocket-powered fighter aircraft developed from the Messerschmitt Me 163 „Komet“ (Comet) towards the end of WW II. Three prototypes were built but never flown under their own power as the rapidly deteriorating military situation in Germany prevented the completion of the test program.
Although the Messerschmitt Me 163 had very short endurance, it had originally been even shorter. In the original design, the engine had only one throttle setting, “full on”, and burned through its fuel in a few minutes. Not only did this further limit endurance, in flight testing, pilots found the aircraft quickly exhibited compressibility effects as soon as they levelled off from the climb and speeds picked up. This led the Reichsluftfahrtministerium (RLM) to demand the addition of a throttle, leading to lengthy delays and a dramatic decrease in fuel economy when throttled.
This problem was addressed in the slightly updated Messerschmitt Me 163C. This featured the same Walter HWK 109-509B or C dual chamber rocket engine already trialled on the Me 163B V6 and V18 prototypes; the main upper chamber („Hauptkammer“) was tuned for high thrust while the lower „Marschofen“ auxiliary combustion chamber was designed for a much lower thrust output (about 400 kgf maximum) for economic cruise. In operation, throttling was accomplished by starting or stopping the main engine, which was about four times as powerful as the smaller one. This change greatly simplified the engine, while also retaining much higher efficiency during cruise. Along with slightly increased fuel tankage, the powered endurance rose to about 12 minutes, a 50% improvement. As the aircraft spent only a short time climbing, this meant the time at combat altitude would be more than doubled.
Throughout development the RLM proved unhappy with the progress on the Me 263 project, and eventually decided to transfer development to Heinrich Hertel at Junkers company. Alexander Lippisch remained at Messerschmitt and retained the support of Waldemar Voigt, continuing development of the Me 163C.
At Junkers, the basic plan of the Me 163C was followed to produce an even larger design, the Junkers Ju 248. It retained the new pressurized cockpit and bubble canopy of the Me 163C, with even more fuel tankage, and adding a new retractable landing gear design. On September 1944 a wooden mock-up was shown to officials. The production version was intended to be powered by the more powerful BMW 109-708 rocket engine in place of the Walter power plant.
Prior to the actual building of the Ju 248, two Me 163Bs, prototype V13 and V18, were slated to be rebuilt. V13 had deteriorated due to weather exposure, so only V18 was rebuilt, but had been flown by test pilot Heini Dittmar at a record-setting 702 mph velocity on July , 1944 and suffered near-total destruction of its rudder surface as a result of high-speed induced compressibility. It is this aircraft that is often identified as the Me 163D, but this aircraft was built after the Ju 248 project had started.
Hertel had hoped to install Lorin ramjet engines, but this technology was still far ahead of its time. As a stopgap measure, they decided to build the aircraft with a „Sondergeräte“ (special equipment) in the form of a „Zusatztreibstoffbehälter“ (auxiliary fuel tank): two 160 l external T-Stoff oxidizer tanks were to be installed under the wings. This would lead to a 10% speed decrease but no negative flight characteristics. Although Junkers claimed the Ju 248 used a standard Me 163B wing, they decided to modify the wing to hold more C-Stoff fuel. This modification was carried out by the Puklitsch firm.
In November 1944, the aircraft was again redesignated as the Messerschmitt Me 263 to show its connection with the Me 163. The two projects also got names – the Ju 248 „Flunder“ (Flounder)) and the Me 263 „Scholle“ (Plaice)). In early 1945, Junkers proposed its own project, the EF 127 „Walli“ rocket fighter, as a competitor to the Me 163C and Me 263.
The first unpowered flight of the Messerschmitt Me 263 V1 was in February 1945. Several more unpowered flights took place that month. The biggest problem had to do with the center of gravity which was restored with the addition of counterweights. Eventually, the production aircraft would have repositioned the engine or the landing gear installation to solve this problem. The landing gear was still non-retractable. The results of those first flights were pricipally satisfying.
Test flights were later stopped because of fuel shortages for the Messerschmitt Bf 110 towplanes. As the Me 263 was not a part of the „Jägernotprogramm“ (Emergency Fighter Programm), it was difficult to get the resources it needed. For the time being the plane was not expected to enter production but further development was allowed. The V2 and V3 were not yet ready. The V2 was to get the retractable landing gear and the V3 would have the armament built in. The next month both the V1 and the V2 had the two-chambered HWK 109-509C installed, correcting the center-of-gravity problems. They flew only as gliders.
In April, American troops occupied the Messerschmitt plant and captured the three prototypes and the mock-up. The V2 was destroyed but another prototype ended up in the US. The rest was handed over to the Russians, who then created their own Mikoyan.Gurewitsch I-270 interceptor (Ref.: 24).

Fighterbomber

Dornier Do 335B-2 (Dragon Models)

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TYPE: Destoyer, Fighter-bomber

ACCOMMODATION: Pilot only

POWER PLANT: Two Daimler-Benz DB 603E-1 liquid-cooled engines, rated at 1,900 hp at 5,905 ft each

PERFORMANCE: 474 mph at 22,000 ft

COMMENT: The Dornier Do 335 „Pfeil“ (Arrow) was a German World-War II heavy fighter built by the Dornier company. The Pfeil’s performance was much better than other twin-engine designs due to its unique push-pull configuration and the lower aerodynamic drag of the in-line alignment of the two engines. It was Germany’s fastest piston-engined aircraft of World War II. The Luftwaffe was desperate to get the design into operational use, but delays in engine deliveries meant that only a handful were delivered before the war ended.
The first 10 Do 335A-0s were delivered for testing in May 1944. By late this year, the Do 335A-1 was on the production line. It was similar to the A-0 but with the uprated DB 603E-1 engines of some 1,800 hp take-off power rating apiece and two underwing hardpoints for additional bombs, drop tanks or guns. It had a maximum speed of 474 mph at 21 300 ft with MW 50 boost, or 426 mph without boost, and climbed to 26, 250 ft in under 15 minutes. Even with one engine out, it reached about 350 mph.
With the worsening of war situation development emphasis in the „Pfeil“ programme switched from the A-series fighter-bomber to the more heavily armed B-series „Zerstörer“ (Destroyer), and during the winter 1944-45 the first Do 335B prototypes were completetd at Oberpfaffenhofen. The initial B-series „Zerstörer“ were essentially similar to the Do 335A-1 apart from armament and the deletion of internal weapon bay, its space being utilized by a supplement fuel tank. The Do 335 V13 had a 15-mm MG 151 cannon in the forward fuselage replaced by 20-mm MG 151s, and was intended to serve as a prototype fort he Do 335B-1, and the Do 335 V14 had this armament supplemented by two 30-mm MK 103 cannon mounted just inboard oft he main undercarriage attachment points, this being the prototype fort he Do 335B-2.
These were destined to be the only B-series prototypes actually completed and flown, although six additional aircraft were under construction at Oberpfaffenhofen when further development was terminated. These were the Do 335 V15 and V16, respectively the second prototype oft he B-1 and B-2 models, the Do 335 V17 which was intended  as a prototype oft he  B-6 two-seat night and bad weather fighter similar to the Do 335 A-6 but posessing the same armament as that oft he B-1; The Do 335 V18 which was to have been the second prototype fort he Do 335B-6, and the  Do 335 V19 and V20 which would have been respectively  prototypes  for the Do 335B-3 and B-7 powered by DB 603LA engines with two stage superchargers, the former being a single-seater similar to the B-2 and the latter being a two-seater similar tot he B-6 (Ref.: 7, 24).

Medium Bomber, Reconnaissance

Heinkel He 119 A-0 (V6), (Valom Models)

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TYPE: Reconnaissance bomber

ACCOMMODATION: Crew of three

POWER PLANT: One Daimler-Benz DB 606A-2, twenty-four-cylinder liquid-cooled coupled engine, rated at 2,350 hp

PERFORMANCE: 367 mph at 14,755 ft

COMMENT: The Heinkel He 119 was an experimental single-propeller monoplane with two coupled engines, developed in Germany. A private venture by Heinkel to test radical ideas by the Günter brothers, the He 119 was originally intended to act as an unarmed reconnaissance bomber capable of eluding all fighters due to its high performance.
Design was begun in the late summer of 1936. A notable feature of the aircraft was the streamlined fuselage, most likely as an evolutionary descendant of the 1932-vintage Heinkel H 70 record-setting single-engined mailplane design, but without the He 70’s protruding canopy-enclosed crew accommodation existing anywhere along the exterior. Instead, the He 119’s forward fuselage featured an extensively glazed cockpit forming the nose itself, heavily framed with many diagonally braced windows immediately behind the propeller spinner’s rear edge. Two of the three-man crew sat on either side of the driveshaft, which ran aft to a “power system”, a coupled pair of Daimler-Benz DB 601 engines mounted above the wing center-section within the fuselage, mounted together within a common mount (the starboard component engine having a “mirror-image” centrifugal supercharger) with a common gear reduction unit fitted to the front ends of each component engine, forming a drive unit known as the Daimler-Benz DB 606, the first German aircraft to use the “high-power” power plant system meant to provide German aircraft with an aviation power plant design of over 2,000 PS output capability.
The DB 606 engine was installed just behind the aft cockpit wall, near the center of gravity, with an enclosed extension shaft passing through the centerline of the extensively glazed cockpit to drive a large four-blade variable-pitch airscrew in the nose. An evaporative cooling system was used on the first aircraft (V1), with the remaining prototypes receiving a semi-retractable radiator directly below the engine to augment cooling during take-off and climb.
Only eight prototypes were completed and the aircraft did not see production, mainly because of the shortages of DB 601 “component” engines to construct the 1,500 kg “power systems” they formed. The first two prototypes were built as land planes, with retractable landing gear. The third prototype (V3) was constructed as a seaplane with twin floats. This was tested at the “Erprobungsstelle Travemünde” military seaplane test facility on the Baltic coast, and was scrapped in 1942 at Heinkel’s factory airfield in the coastal Rostock-Schmarl community, then known as Marienehe.
On November 1937, the fourth prototype (V4) made a world class-record flight in which it recorded an airspeed of 314 mph, with a payload of 1,000 kg, over a distance of 1,000 km. The four remaining prototypes were completed during the spring and early summer of 1938, the V5 and V6 being A-series production prototypes for the reconnaissance model, and the V7 and V8 being B-series production prototypes for the bomber model.
These four aircraft were three-seaters with a defensive armament of one 7.92 mm MG 15 machine gun in a dorsal position, V7 and V8 having provision for a normal bombload of three 250 kg bombs or maximum bombload of 1,000 kg. V7 and V8 were sold to Japan in May 1940, and extensively studied; the insights thus gained were used in the design of the Yokosuka R2Y1 “Keiun” The remaining prototypes served as engine test-beds, flying with various prototype versions of the DB 606 and DB 610 (twinned Daimler-Benz DB 605) and the experimental DB 613 (twinned Daimler-Benz DB 603).
In 1944, a high-speed bomber development, designed as a private venture by Heinkel to test radical ideas by the Günter brothers, was the Heinkel He 519. It was designed to use the 24-cylinder Daimler-Benz DB 613, but the aircraft remained a concept and was abandoned at the end of the war. (Ref.: 24).