Dornier Do 335

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Do 335 Pfeil
Dornier Pfeil2.jpg
The only surviving Do 335 (VG+PH) at the Steven F. Udvar-Hazy Center near Washington, D.C.'s Dulles Airport
Role Fighter-bomber
Manufacturer Dornier Flugzeugwerke
First flight 26 October 1943
Introduction 1944
Retired 1945
Status Retired
Primary user Luftwaffe
Produced 1944–1945
Number built 37[1]

The Dornier Do 335 Pfeil ("Arrow") was a World War II heavy fighter built by the Dornier company. The two-seater trainer version was called Ameisenbär ("anteater"); 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 Nazi Germany's fastest piston-engined aircraft of World War II.[2][page needed] 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.

Design and development[edit]

The origins of the Do 335 trace back to World War I when Claude Dornier designed a number of flying boats featuring remotely driven propellers and later, due to problems with the drive shafts, tandem engines. Tandem engines were used on most of the multi-engine Dornier flying boats that followed, including the highly successful Do J Wal and the gigantic Do X; the remote propeller drive, intended to eliminate parasitic drag from the engine entirely, was tried in the innovative but unsuccessful Do 14, and elongated, tubular drive shafts as later used in the Do 335 saw use in the rear engines of the four-engined, twinned tandem-layout Do 26 flying boat.

There are many advantages to this design over the more traditional system of placing one engine on each wing, the most important being power from two engines with the frontal area (and thus drag) of a single-engine design, allowing for higher performance, it also keeps the weight of the twin powerplants near, or on, the aircraft centerline, increasing the roll rate compared to a traditional twin. In addition, a single engine failure does not lead to asymmetric thrust, and in normal flight there is no net torque, so the plane is easy to handle; the choice of a full "four-surface" set of cruciform tail surfaces in the Do 335's rear fuselage design, included a ventral vertical fin–rudder assembly to project downwards from the extreme rear of the fuselage, in order to protect the rear propeller from an accidental ground strike on takeoff. The presence of the rear pusher propeller also mandated the provision for an ejection seat for safe escape from a damaged aircraft, and designing the rear propeller and dorsal fin mounts to use explosive bolts to jettison them before an ejection was attempted — as well as twin canopy jettison levers, one per side[3] located to either side of the forward cockpit interior just below the sills of the five-panel windscreen's sides, to jettison the canopy from atop the cockpit before ejection.[4]

In 1939, Dornier was busy working on the P.59 high-speed bomber project, which featured the tandem engine layout. In 1940, he commissioned a test aircraft, closely modeled on the airframe of the early versions of the Dornier Do 17 bomber but only 40% of the size of the larger bomber, with no aerodynamic bodies of any sort on the wing panels (the original Do 17 had twin engine nacelles on its wings) and fitted with a retractable tricycle landing gear to validate his concept for turning the rear pusher propeller with an engine located far away from it, through the use of a long tubular driveshaft; this aircraft, the Göppingen Gö 9, showed no unforeseen difficulties with this arrangement, but work on the P.59 was stopped in early 1940 when Hermann Göring[citation needed] ordered the cancellation of all projects that would not be completed within a year or so.

In May 1942, Dornier submitted an updated version with a 1,000 kg (2,200 lb) bombload as the P.231, in response to a requirement for a single seat, Schnellbomber-like high-speed bomber/intruder. The P.231 proposal was selected as the winner after beating rival designs from Arado, Junkers, and Blohm & Voss development contract was awarded, by the RLM issuing the Dornier firm the airframe approval number 8-335, for what would become known as the Do 335. In autumn 1942, Dornier was told that the Do 335 was no longer required, and instead a multi-role fighter based on the same general layout would be accepted; this delayed the prototype delivery as it was modified for the new role.

Do-335s on the apron at Oberpfaffenhofen at the war's end, including unfinished two-seat versions

The use of a nose-mount annular radiator for the forward engine (much like a Jumo 211-powered Ju 88, or Jumo 213-powered Focke-Wulf Fw 190D-9) and a ventral-fuselage mount airscooped radiator installation for cooling the rear engine (appearing like that on a P-51 Mustang) was distinctive; when fitted with DB 603A engines delivering 1,750 PS (1,287 kW, 1,726 hp) at takeoff it had a pair of the largest displacement (at 44.52 litres) inverted V12 aircraft engine design mass-produced during the Third Reich's existence. The Do 335 V1 first prototype, bearing the Stammkennzeichen (factory radio code) of CP+UA, flew on 26 October 1943 under the control of Flugkapitän Hans Dieterle, a regular Heinkel test pilot and later primary Dornier test pilot. However, several problems during the initial flight of the Do 335 would continue to plague the aircraft through most of its short history. Issues were found with the weak landing gear and with the main gear's wheel well doors, resulting in them being removed for the remainder of the V1's test flights; the Do 335 V1 made 27 flights, flown by three different pilots. During these test flights the V2 (W.Nr 230002), Stammkennzeichen CP+UB was completed and made its first flight on 31 December 1943, again under the control of Dieterle. New to the V2 were upgraded DB 603A-2 engines, and several refinements learned from the test flights of the V1 as well as further windtunnel testing. On 20 January 1944, the Do 335 V3 (W.Nr. 230004), Stammkennzeichen CP+UC was completed and flown for its first time by Werner Altrogge. The V3 was powered by the new pre-production DB 603G-0 engines which could produce 1,900 PS (1,400 kW) at take-off and featured a slightly redesigned canopy which included twin rear-view mirrors in blisters, one in each of two matching side panels of the well-framed, eleven-panel main canopy's openable section. Following the flights of the V3, in mid January 1944, RLM ordered five more prototypes (V21–V25), to be built as night fighters. By this time, more than 60 hours of flight time had been put on the Do 335 and reports showed it to be a good handling, but more importantly, very fast aircraft, described by Generalfeldmarschall Erhard Milch himself as "...holding its own in speed and altitude with the P-38 and it does not suffer from engine reliability issues". Thus 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.

On 23 May 1944, Hitler, as part of the developing Jägernotprogramm (Emergency Fighter Program) directive, which took effect on 3 July, ordered maximum priority to be given to Do 335 production; the main production line was intended to be at Manzell, but a bombing raid in March destroyed the tooling and forced Dornier to set up a new line at Oberpfaffenhofen. The decision was made, along with the rapid shut-down of many other military aircraft development programs, to cancel the Heinkel He 219 night fighter, which also used the DB 603 engines (in well-unitized installations), and use its production facilities for the Do 335 as well. However, Ernst Heinkel managed to delay, and eventually ignore, its implementation, continuing to produce examples of the He 219A.

At least 16 prototype Do 335s were known to have flown (V1–V12, W.Nr 230001-230012 and Muster-series prototypes M13–M17, W.Nr 230013-230017) on a number of DB603 engine subtypes including the DB 603A, A-2, G-0, E and E-1; the first preproduction Do 335 (A-0s) starting with W.Nr 240101, Stammkennzeichen VG+PG, were delivered in July 1944. Approximately 22 preproduction aircraft were thought to have been completed and flown before the end of the war, including approximately 11 A-0s converted to A-11s for training purposes. One such aircraft was transferred to the Royal Aircraft Establishment in Farnborough, and later, after a rear-engine fire burnt through the elevator controls during a flight, crashed onto a local school.[5]

Flight tests[edit]

Do 335 tested in the US, and today the only surviving example

The first 10 Do 335 A-0s were delivered for testing in May. By late 1944, the Do 335 A-1 was on the production line. It was similar to the A-0 but with the uprated DB 603E-1 engines of some 1,324 kW (1,800 PS) take-off power rating apiece on 87 octane "B4" lignite-derived synthetic fuel,[6] and two underwing hardpoints for additional bombs, drop tanks or guns, it had a maximum speed of 763 km/h (474 mph) at 6 500 m (21 300 ft) with MW 50 boost, or 686 km/h (426 mph) without boost, and climbed to 8 000 m (26 250 ft) in under 15 minutes. Even with one engine out, it reached about 563 km/h (350 mph).[citation needed]

Delivery commenced in January 1945; when the United States Army overran the Oberpfaffenhofen factory in late April 1945, only 11 Do 335 A-1 single-seat fighter-bombers and two Do 335 A-12 trainers had been completed.

French ace Pierre Clostermann claimed the first Allied combat encounter with a Pfeil in April 1945, he describes leading a flight of four Hawker Tempests from No. 3 Squadron RAF over northern Germany, when he intercepted a lone Do 335 flying at maximum speed at treetop level. Detecting the British aircraft, the German pilot reversed course to evade. Despite the Tempests' considerable low altitude speed, the Royal Air Force fighters were not able to catch up or even get into firing position.[7]

Variants[edit]

Dornier Pfeil
Built
  • Do 335 A-0 : 10 pre-production aircraft.
  • Do 335 A-1 : Single-seat fighter-bomber aircraft.
Proposed
  • Do 335 A-2: single-seat fighter-bomber aircraft with new weapon aiming systems, later proposed longer wing and updated DB603L engines of at least 1,471 kW (2,000 PS) output apiece.
  • Do 335 A-3: single-seat reconnaissance aircraft built from A-1 aircraft, later proposed with longer wing.
  • Do 335 A-4: single-seat reconnaissance aircraft with smaller cameras than the A-3
  • Do 335 A-5: single-seat night fighter aircraft, later night and bad weather fighter with enlarged wing and DB603L engines.
  • Do 335 A-6: two-seat night fighter aircraft, with completely separate second cockpit located above and behind the original.
  • Do 335 A-7: A-6 with longer wing.
  • Do 335 A-8: A-4 fitted with longer wing.
  • Do 335 A-9: A-4 fitted with longer wing, DB603L engines and pressurized cockpit.
  • Do 335 B-1: abandoned in development.
  • Do 335 B-2: single-seat destroyer aircraft. Fitted with 2 additional MK 103 in the wings and provision to carry two standard Luftwaffe 300 litre (80 US gal) drop tanks.
  • Do 335 B-3: updated B-1 but with longer wing.
  • Do 335 B-4: update of the B-1 with longer wing, DB603L engine.
  • Do 335 B-6: night fighter.
  • Do 335 B-12: dual-seat trainer version for the B-series aircraft.
  • Do 435: a Do 335 with the redesigned, longer wing. Allied intelligence reports from early May 1945 mention spotting a Do 435 at the Dornier factory airfield at Lowenthal.
  • Do 535: actually the He 535, once the Dornier P254 design was handed over to Heinkel in October 1944; fitted with jet engine in place of rear piston engine[8]
  • Do 635: twin-fuselaged long-range reconnaissance version. Also called Junkers Ju 635 or Do 335Z. Mock up only.
  • Do P 256: turbojet nightfighter version, with two podded HeS 011 turbojet engines,[9] based on Do 335 airframe.

Surviving aircraft[edit]

Only one Do 335 survives, the second preproduction Do 335 A-0, designated A-02, with construction number (Werknummer) 240 102, and factory radio code registration, or Stammkennzeichen, of VG+PH. The aircraft was assembled at the Dornier plant in Oberpfaffenhofen, Bavaria on 16 April 1945, it was captured by Allied forces at the plant on 22 April 1945. VG+PH was one of two Do 335s to be shipped to the United States aboard the Royal Navy escort carrier HMS Reaper, along with other captured German aircraft, to be used for testing and evaluation under a USAAF program called "Operation Lusty". One Do 335 (registration FE-1012) went to the USAAF and was tested in early 1946 at Freeman Field, Indiana, USA, its fate is not recorded.

VG+PH went to the Navy for evaluation and was sent to the Test and Evaluation Center, Patuxent River Naval Air Station, Maryland, USA. Following testing from 1945 to 1948, the aircraft languished in outside storage at Naval Air Station Norfolk. In 1961, it was donated to the Smithsonian's National Air Museum, though it remained in deteriorating condition at Norfolk for several more years before being moved to the National Air and Space Museum's storage facility in Suitland, Maryland. In October 1974, VG+PH was returned to the Dornier plant in Oberpfaffenhofen, Germany (then building the Alpha Jet) for a complete restoration. In 1975, the aircraft was restored by Dornier employees, many of whom had worked on the airplane originally, they were surprised that the explosive charges built into the aircraft to blow off the dorsal fin and rear propeller prior to pilot ejection were still installed and active 30 years later.[citation needed]

Following restoration the completed Do 335 was displayed at the Hannover, Germany Airshow from 1 May to 9 May 1976. After the air show, the aircraft was loaned to the Deutsches Museum in Munich, where it was on display until 1988, when it was shipped back to Silver Hill, Maryland. VG+PH can be seen today in the Steven F. Udvar-Hazy Center of the National Air and Space Museum alongside other unique late-war German aircraft, such as the only known example of the Arado Ar 234 B-2 Blitz jet reconnaissance-bomber, and the fully restored fuselage and tail surfaces of the only complete surviving Heinkel He 219A Uhu (Eagle-Owl) night fighter (the wings and engines/nacelles are still undergoing restoration).[10][11]

Specifications (Do 335 A-1)[edit]

Dornier Do 335.svg

Data from Aircraft of the Third Reich Volume one,[12] Century of Flight : Dornier Do 335 Pfeil[13]

General characteristics

  • Crew: 1
  • Length: 13.85 m (45 ft 5 in)
  • Wingspan: 13.8 m (45 ft 3 in)
  • Height: 5 m (16 ft 5 in)
  • Wing area: 38.5 m2 (414 sq ft)
  • Airfoil: root: NACA 23018-630; tip: NACA 23012-635[14]
  • Empty weight: 7,260 kg (16,006 lb)
  • Gross weight: 9,600 kg (21,164 lb)
A-6 10,085 kg (22,234 lb)
  • Fuel capacity: 1,230 l (320 US gal; 270 imp gal) main fuel tank (single-seat) with various extra tankage in the weapons bay and wings, depending on variant
  • Powerplant: 2 × Daimler-Benz DB 603E-1 V-12 inverted liquid-cooled piston engines for take-off
1,417 kW (1,900 hp) at 1,800 m (5,900 ft)
  • Propellers: 3-bladed VDM, 3.5 m (11 ft 6 in) diameter constant-speed tractor and pusher propellers

Performance

  • Maximum speed: 763 km/h (474 mph; 412 kn) at 6,500 m (21,300 ft)
A-6 690 km/h (430 mph; 370 kn) at 5,300 m (17,400 ft)
  • Cruise speed: 685 km/h (426 mph; 370 kn) at 7,200 m (23,600 ft)
  • Economical cruise speed: 452 km/h (281 mph; 244 kn) at 6,000 m (20,000 ft)
  • Range: 1,395 km (867 mi; 753 nmi) on full internal fuel at max. continuous power
2,060 km (1,280 mi; 1,110 nmi) at economical cruise power
  • Service ceiling: 11,400 m (37,400 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 55 seconds ; 8,000 m (26,000 ft) in 14 minutes 30 seconds

Armament

  • Guns: 1 × engine mounted 30 mm (1.18 in) MK 103 cannon with 70 rpg plus 2 × 20 mm (0.79 in) MG 151/20 cowl-mount, synchronized autocannon with 200 rpg
  • Bombs: Up to 1,000 kg (2,200 lb) bombload in internal weapons bay and two underwing pylons

See also[edit]

Related development

Aircraft of comparable role, configuration and era

Related lists

References[edit]

Notes
  1. ^ Wilson 1998, p. 56.
  2. ^ Smith, J. Richard. Dornier Do 335: The Luftwaffe's Fastest Piston-Engine Fighter (Classic Publications, 2007).
  3. ^ NASM's restored Do 335A's cockpit, displaying the starboard-side example of the twin canopy jettison levers
  4. ^ "Century of Flight - German Aircraft of World War Two - Dornier Do 335 Pfeil". www.century-of-flight.net. Century of Flight.
  5. ^ Smith, Joshua. "Farnborough Air Sciences Trust Museum uncovers secrets behind a plane which crashed on Cove school". GetHampshire. Aldershot News & Mail Series. Archived from the original on 1 February 2016. Retrieved 1 February 2016.
  6. ^ Archived Fischer-Tropsch.org pdf file (extract) pp.119–120. Retrieved:27 March 2019.
  7. ^ Clostermann, Pierre, The Big Show, pp. 273–74
  8. ^ Christopher, John. The Race for Hitler's X-Planes (The Mill, Gloucestershire: History Press, 2013), p.179.
  9. ^ Schick, Walter; Meyer, Ingolf (1997), Luftwaffe Secret Projects: Fighters, 1939–45, Leicester: Midland, p. 123.
  10. ^ "Dornier Do 335 A-0 Pfeil (Arrow)". Smithsonian National Air and Space Museum. Retrieved 21 November 2016.
  11. ^ Lerche, Hans-Werner (May 1976). "Der letzte Flug der Do 335". Luftfahrttechnisches Museum Rechlin (in German). Retrieved 21 November 2016.
  12. ^ Green, William (2010). Aircraft of the Third Reich Volume one. London: Crecy. pp. 288–298. ISBN 9781900732062.
  13. ^ "Dornier Do 335 Pfeil". Century of Flight. Retrieved 21 November 2016.
  14. ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
Bibliography
  • Angelucci, Enzo. The Rand McNally Encyclopedia of Military Aircraft, 1914–1980. San Diego, California: The Military Press, 1983. ISBN 0-517-41021-4.
  • Wilson, Stewart. Aircraft of WWII. Fyshwick, ACT, Australia: Aerospace Publications Pty Ltd., 1998. ISBN 1-875671-35-8.

External links[edit]


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