Do 335 Pfeil | |
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Role | Fighter-bomber |
Manufacturer | Dornier Flugzeugwerke |
First flight | October 1943 |
Introduced | 1944 |
Primary user | Luftwaffe |
Number built | 37[1] |
Contents
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Development
The origins of the Do 335 trace back to World War I when Claudius 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 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 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 design, allowed the 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.
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 to validate his concept for turning the rear pusher propeller with an engine located far away from it and using a long 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 which 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 high-speed bomber/intruder. P.231 was selected as the winner after beating rival designs from Arado, Junkers, and Blohm & Voss development contract was awarded 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.
Fitted with DB 603A engines delivering 1,750 PS (1,287 kW, 1,726 hp) at takeoff, 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. The pilots were surprised at the speed, acceleration, turning circle, and general handling of the type; it was a twin that flew like a single. 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 gear doors, resulting in them being removed for the remainder of V1 flights. V1 made 27 flights, flown by three different pilots. During these test flights 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 DB603 A-2 engines, and several refinements learned from the test flights of V1 as well as further windtunnel testing. On 20 January 1944, V3 (W.Nr. 230004),Stammkennzeichen CP+UC was completed and flown for its first time by Werner Altrogge. V3 was powered by the new DB603 G-0 engines which could produce 1,900 PS (1,400 kW) at take-off and featured a slightly redesigned canopy which included rear-view mirrors in blisters, one in each of two matching side panels of the main canopy. 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 be a good handling, but more importantly, very fast aircraft, described by Miltch himself as "...holding its own in speed and altitude with the P-38 and 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 Jägernotprogramm directive, ordered maximum priority to be given to Do 335 production. The main production line was intended to be at Manzel, 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, and use its production facilities for the Do 335 as well. However, Ernst Heinkel managed to delay, and eventually ignore, its implementation.
At least 16 prototype Do 335s were known to have flown (V1–V12, W.Nr 230001-230012 and Müster-series prototypes M13–M17, W.Nr 230013-230017) on a number of DB603 engines including the DB603A, 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.
Flight tests
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. This was similar to the A-0 but with the uprated DB 603 E-1 engines and two underwing hardpoints for additional bombs, drop tanks or guns. It was capable of 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 able to climb to 8,000 m (26,250 ft) in under 15 minutes. Even with one engine out, it could reach about 563 km/h (350 mph).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. In his book The Big Show (pages 273-274) he describes leading a flight of four Hawker Tempests from No. 3 Squadron RAF over northern Germany, 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 Tempest's considerable low altitude speed, the RAF fighters were not able to catch up or even get into firing position.
Variants
- Do 335 A-0 : 10 pre-production aircraft.
- Do 335 A-1 : Single-seat fighter-bomber aircraft.
- Do 335 A-2 : Proposed single-seat fighter-bomber aircraft with new weapon aiming systems, later proposed longer wing and updated DB603L engines.
- Do 335 A-3 : Proposed single-seat reconnaissance aircraft built from A-1 aircraft, later proposed with longer wing.
- Do 335 A-4 : Proposed single-seat reconnaissance aircraft with smaller cameras than the A-3
- Do 335 A-5 : Proposed single-seat night fighter aircraft, later night and bad weather fighter with enlarged wing and DB603L engines.
- Do 335 A-6 : Proposed two seat night fighter aircraft.
- Do 335 A-7 : Proposed A-6 with longer wing.
- Do 335 A-8 : Proposed A-4 fitted with longer wing.
- Do 335 A-9 : Proposed A-4 fitted with longer wing, DB603L engine 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 two 315 auxiliary fuel tanks.
- Do 335 B-3 : Proposed updated B-1 but with longer wing.
- Do 335 B-4 : Proposed update of the B-1 with longer wing, DB603L engine.
- Do 335 B-12: Proposed 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 make a report of a spotted 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.
- Do 635 : Proposed long-range reconnaissance version. Also called Junkers Ju 635 or Do 335Z. Mock up only.
- Do P 256: Proposed turbojet nightfighter version, with two podded He S011 engines,[2] based on Do 335 airframe. Not built.
Survivors
Only one Do 335 survives today. The aircraft was the second preproduction Do 335 A-0, designated A-02, with construction number (Werknummer) 240102, and factory radio code registration, or Stammkennzeichen, of VG+PH. The aircraft was assembled at Dornier's plant in Oberpfaffenhofen (southern Germany) on 16 April 1945. It was captured by Allied forces at the plant on 22 April 1945. The aircraft was test flown from a grass runway at Oberwiesenfeld, near Munich, to Cherbourg, France while escorted by two P-51s. The Do 335 was easily able to out distance the escorting Mustangs and arrived at Cherbourg 45 minutes before the P-51s. 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 Sea Horse". One Do 335 (registration FE-1012) went to the USAAF and was tested in early 1946 at Freeman Field, Indiana. 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. 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 the National Air & 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 amazed to find that the explosive charges built into the aircraft to blow off the tail fin and rear propeller in the event of an emergency were still on the aircraft and active 30 years later.
Following restoration the completed Do 335 was displayed at the Hanover, Germany Airshow from 1 May to 9 May 1976. After the air show, the aircraft was lent to the Deutsches Museum in Munich where it was on display, without a swastika on the dorsal vertical tail in accordance with German law, until 1986, 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 & Space Museum alongside other unique late-war German aircraft such as the only known example of the Arado Ar 234B-2 Blitz jet recon-bomber, and the only surviving Heinkel He 219A Uhu (Eagle-Owl) night fighter's fully restored fuselage and tail surfaces is on display as an assembled unit, as the wings and engines/nacelles of the surviving He 219A there are still undergoing restoration as of Oct 2009.
Specifications (Do 335 A-0)
General characteristics- Crew: 1, pilot
- Length: 45 ft 5 in (13.85 m)
- Wingspan: 45 ft 1 in (13.8 m)
- Height: 15 ft (4.55 m)
- Wing area: 592 ft² (55 m²)
- Empty weight: 11,484 lb (5,210 kg)
- Max takeoff weight: 19,500 lb (8,590 kg)
- Powerplant: 2× Daimler-Benz DB 603A 12-cylinder inverted engines, 1,287 kW, 1,726 hp (1,750 PS) each
- Maximum speed: 474 mph (765 km/h)
- Combat radius: 721 mi (1,160 km (half load))
- Service ceiling: 37,400 ft (11,400 m)
- 1 × 30 mm (1.18 in) MK 103 cannon (as forward engine-mounted Motorkanone)
- 2 × 20 mm MG 151 cannons
- Up to 1,000 kg (2,200 lb) bombload
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