TYPE: Night-fighter

ACCOMMODATION:  Crew of four

POWER PLANT: Two Daimler-Benz DB 603A liquid-cooled engines, rated at 1,849 hp each at 6,900 ft

PERFORMANCE: 350 mph at 18,700 ft

COMMENT: The Dornier Do 217 was a bomber used by the German Luftwaffe during World War II. It was a more powerful development of the Dornier Do 17, known as the Fliegender Bleistift (flying pencil). Designed in 1937-38 as a heavy bomber but not meant to be capable of the longer-range missions envisioned for the larger Heinkel He 177 Greif (Griffon), the Do 217’s design was refined during 1939 and production began in late 1940. It entered service in early 1941 and by the beginning of 1942 was available in significant numbers. The Do 217 was also converted to become a night fighter and saw considerable action in the Defence of the Reich campaign until late in the war.
In 1941, with Germany under increased night-time attack by RAF Bomber Command and with shortages of the Messerschmitt Bf 110 and the preferred Junkers Ju 88C night fighters, it was decided to supplement the night-fighter force with a version of the Dornier Do 217 E, despite its much greater size and 15-ton weight. This aircraft, the Do 217 J, was fitted with a new “solid” nose with four forward firing 20 mm MG FF cannon and four 7.92 mm machine guns.
By October 1940, the production of heavy night fighters and night fighters such as the Do 217 and Ju 88, had been discussed comprehensively and by 5 November 1941 these discussions had been concluded. On November 1941 the Technische Amt (T.A.) had ordered the Dornier Do 217E bomber fleet to be withdrawn in accordance with a decision made earlier that year on May. Dornier designated the subject of their new project the Dornier Do 217 Z, later renamed the Do 217 J. Two versions were ordered as Dornier Do 217J- 1 and Do 217J-2 and delivered to night fighter groups began in early 1942
Complaints were made by crews about the performance of the Dornier in comparison to other German types. On 12 May 1942 Erhard Milch ordered that Dornier cease all night fighter design. It was decided that the Ju 88 series only (Ju 88 C-6) would continue to be developed and serve as a heavy night fighter. Strangely, the order was not passed onto the Dornier design team who continued to produce the Do 217N variant
After testing was satisfied the two variants, the Do 217N-1 and Do217N-2, which had two sub-variants, were fitted with FuG 202. The Do 217N-1 variants were given two sub-variants which were to follow the design of the Do 217E-2/E-4 and the Do 217J-1/J-2 with emphasis on range and endurance. Extra fuel tanks were added to the empty bomb bay. For operations over water the heavy night fighters were fitted with lifeboats and radio transmitters. The FuG X with TZG 10 and FuG 16. IFF equipment was the FuG 25s. The Do 217N also had the FuG 101 radio altimeter, blind flying equipment FuB1 2 and PeilG V. AI search radar was the FuG 202. The no longer needed bomb release gear remained, bringing the aircraft up to 33,000 lb on take-off, so it was barely able to reach 24,300 ft. Fuel consumption lightened the load, and the Dornier could reach a maximum operational ceiling of 27,600 ft. The speed of the Do 217N was a maximum of 500 kilometres per hour (270 kn) at 6,000 metres (20,000 ft). The Do 217N-2 was much improved, as it was much lighter and refined.
Overall the Dornier Do 217N-1 was an initial production of the Do 217J-1 version. Powered by a Daimler-Benz DB 603 it had similar armament to Do 217 J-2, retaining defensive armament. Entered service in April 1943. Some modified with dorsal and ventral guns replaced by wooden fairings as Do 217 N-1/U1, conversion with Schräge Musik arrangement of four upward-firing 20 mm MG 151s as Do 217 N-1/U3. About 240 aircraft were built (Ref: 24).

TYPE: Night fighter

ACCOMMODATION: Pilot and radar operator/Navigator

POWER PLANT: Two Daimler-Benz DB 603G liquid-cooled engines, rated at 1,776 hp each

PERFORMANCE: 420 mph at 23,000 ft

COMMENT: The Heinkel He 219 Uhu (“Eagle-Owl”) was a night fighter designed and produced by the German aircraft manufacturer Heinkel. It primarily served with the Luftwaffe in the later stages of the Second World War.
Work on the He 219 begun in mid 1940 as a multi-purpose aircraft designated P.1055. It was a relatively sophisticated design that possessed a variety of innovations, including a pressurized cockpit, twin ejection seats and remotely controlled defensive gun turrets. The P.1055 was initially rejected by the Reichsluftfahrtministerium (RLM – the German Aviation Ministry), but Heinkel promptly reconfigured it as a night fighter, designated P.1060. In this capacity, it was equipped with a FuG 220 Lichtenstein SN-2 advanced VHF-band intercept radar (also used on the Junkers Ju 88G and Messerschmitt Bf 110G night fighters). The Heinkel He 219A was also the first operational military aircraft to be equipped with ejection seats and the first operational German aircraft to be equipped with tricycle landing gear  The prototype performed its maiden flight on 6 November 1942.
Both the development and production of the He 219 were protracted due to various factors, including political rivalries between General J. Kammhuber, commander of the German night fighter forces, Ernst Heinkel, the manufacturer and Field Marshal E. Milch, responsible for aircraft construction in the RLM. Other aircraft programmes, such as the Junkers Ju 188, Donier Do 335 Pfeil and Focke-Wulf Ta 154 Moskito, competed for attention and resources; Milch advocated for these programmes over the He 219. Furthermore, the aircraft was relatively complicated and expensive to build, as were the powerful Daimler-Benz DB 610 V-12 inline engines that powered it. Nevertheless, the He 219 made its combat debut on June 1943 and was quickly recognised for its value as a night fighter, even being allegedly effective against the Royal Air Force’s de Havilland Mosquito fighter-bombers.
On 25 May 1944, production of the He 219 was officially terminated. Had the He 219 ever become available to the Luftwaffe in large quantities, it is plausible that it could have had a significant effect against the strategic night bombing offensive conducted against Germany by the Royal Air Force (RAF); however, only 268 aircraft across all models were ever completed and thus the type only saw limited service between 1943 and 1945. Major E.-W. Modrow was the leading night fighter ace on the He 219, having been credited with 33 of his 34 night air victories on the type.
The last major production version was the Heinkel He  219A-7 with improved, unitized 1,776 hp Daimler-Benz DB 603E engines. The A-7 typically had two 20 mm MG 151/20 cannon in the wing roots (inboard of the propeller arcs), two 20 mm MG 151/20 in the ventral weapons bay and two 30 mm (1.18 in) MK 108s as rear-fuselage dorsal mount, upwards-firing Schräge Musik offensive ordnance. Production of 210 aircraft was to start November/December 1944, but only six aicraft have been produced, one aircraft was delivered to the I/NJG 1 (Ref.: 24).

TYPE: Night- and all-weather fighter

ACCOMMODATION:  Pilot and Radar operator/Navigator

POWER PLANT: Two Daimler-Benz DB 603E1-cooled piston engines with two-stage superchargers, rated at 1,900 hp at 5,900 ft

PERFORMANCE:  474 mph at 21,300 ft

COMMENT: The Dornier Do 335 Pfeil (Arrow) was a heavy fighter built by Dornier for the German Luftwaffe during World War II. The Pfeil’s performance was predicted to be better than other twin-engine designs due to its unusual push-pull configu­ration and the lower aerodynamic drag of the in-line alignment of the two engines. It was Nazi 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 Do 335 was originally designed as a Schnellbomber. It could reach speeds of almost 500 mph in level flight, and could outrun most of the military aircraft in service at the time, with only first generation jet fighters being faster. The front engine of the Pfeil was the Daimler-Benz DB 605, and the rear one the DB 605 QA
The first 10 Dornier 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.
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 of the Dornier Do 335B-1 and Dornier Do 335B-2 models, the Do 335 V17 which was intended  as a prototype of the  B-6 two-seat night and bad weather fighter similar to the 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 to the B-6.
The two-seated night-fighter Dornier Do 335B-6 was  provided with a FuG 218 Neptun radar system with Hirschgeweih ( stag’s antlers) eight-dipol array with shorter elements than  the previous 90 MHz SN-2 radar (Ref.: 7, 24).

TYPE: Night- and bad-weather fighter

ACCOMMODATION:  Pilot and radar-operator/navigator

POWER PLANT: Two Daimler-Benz DB 603g liquid-cooled engines, rated at 1,726 hp each

PERFORMANCE: 472 mph at 27.800 ft

COMMENT: As early as 1940, the Messerschmitt design bureau concerned itself with the idea of fusing two fighters into a single airframe to provide a considerable increase in range and payload. The work was based on a RLM edict to simplify the number of combat aircraft to a few basic models.
Known as Messerschmitt Me 109Z Zwilling (twin) and Messerschmitt Me 609, the layouts were primarily intended as Zerstörer (Destroyer), Schnellbomber (Fast bomber or Nachtjäger (Night fighter). Following detailed examinations, the most suitable solution capable of early production indicated the use of a Daimler-Benz DB 605A-powered Messerschmitt Me 109G. A considerable performance increase, however, was to be expected if  2,000 hp Junker Jumo 213 engines were installed, requiring only a few alteration to incorporate complete major components of the standard aircraft. The modifications were limited mainly to the need of a completely new constant –cord wing center section and tailplane that simplified manufacture. Besides relocation of the undercarriage attachment points and the use of larger wheels, the ailerons and outboard leading-edge slots were lengthened and auxiliary fuel tanks were installed. In the course of development work on the twin aircraft, the Messerschmitt Me 309 was also considered and resulted in the Messerschmitt Me 609 destroyer, fast bomber and night fighter. The more powerful engine intended for the Messerschmitt Me 609 led to improvements in flight performance.
For the Night fighter version a FuG 217V/R “Neptun” radar with smal “Hirschgeweih” (Stag’s Antlers) aerial array was provided. These were mounted at the wingtips close to the leading edge. When all work on the unsuccessful Messerschmitt Me 309 was stopped all further effort on the Me 609 was cancelled (Ref.: 24).

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).

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).

TYPE: Two-seat all weather and night interceptor

ACCOMMODATION: Pilot and radar operator

POWER PLANT: Two Daimler-Benz DB 603A-2, rated at 1,726 hp each

PERFORMANCE: 400 mph at 17,400 ft

COMMENT: The Dornier Do 335 “Pfeil” (“Arrow”) was a WW II heavy fighter built by the Dornier Company. The Do 335s 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 Luftwaffe fastest piston-engine 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.
In early 1944 the Do 335 was scheduled to begin mass construction, with the initial order of 120 preproduction aircraft to be manufactured by DWF (Dornier-Werke Friedrichshafen) to be completed no later than March 1946. This number included a number of bombers, destroyers (heavy fighters), and several yet to be developed variants. At the same time, DWM (Dornier-Werke München) was scheduled to build over 2000 Do 335s in various models, due for delivery in March 1946 as well.
While the Dornier Do 335A-0 assembly line at Oberpfaffenhofen was struggling to overcome delays in deliveries of power plants, airscrews, radio equipment and sub-contracted components and assemblies, a number of “Versuchs” (Test) machines for other “Pfeil” subtypes joined the test programme, these including the first two seat models, the Do 335A-6 bad-weather and night interceptor and the Do 335A-12 trainer..
The Dornier Do 335 V10 was the first prototype for the Do 335A-6 radar-equipped two set all weather and night interceptor in which a second cockpit for the radar operator was inserted aft and above the normal cockpit. In order to provide space for the additional cockpit the fuel tankage was drastically revised, the weapon bay being deleted and its space utilized for fuel, fuselage tankage being increased substantially. Cannon armament remained unchanged, but a FuG 101a radio altimeter was
introduced together with FuG 217J-2 “Neptun” intercept radar with wing-mounted antennae. Exhaust flame damping tubes for the fore and aft engines added their measure of drag to that provides by the second cockpit and the radar antennae, and normal loaded weight increased by app. 500 kg. Performance accordingly fell by 10 per cent, but whereas the Do 335 V10 had Daimler-Benz DB 603A-2 engines, the production Do 335 A-6 was intended to have DB 603E engines with provision for methanol-water injection (MW 50) for power boosting below the rated altitude of power plants. Provision was to be made in the wings for two MW 50 tanks, power being boosted to 2,400 hp at sea level per engine.
Production of the Dornier Do 335A-6 night and all-weather fighter had been transferred to the Heinkel factory at Vienna, but despite high priority allocated to the program, circumstances prevented the necessary jigs and tools being assembled (Ref: 7, 12).