/Airplanes/Axis/Germany/02-Fighter-Bombers/Do-335/Do-335A-1.htm | Update: 25-03-2019


Dornier Do-335A-1 Pfeil

Fighter, Fighter-Bomber
1 or 2
Dornier Flugzeugwerke GmbH
37; Do 335V: 14 , Do 335A-0: 10, Do 335A-1: 11, Do 335A-12: 2 (1944–1945)
26 October 1943 (Prototype)


Preproduction. Fighter / fighter bomber.
Production model. Single-seat fighter-bomber aircraft.
Single-seat fighter-bomber aircraft with new weapon aiming systems, later proposed longer wing and updated DB603L engines.
Single-seat reconnaissance aircraft built from A-1 aircraft, later proposed with longer wing.
Single-seat reconnaissance aircraft with smaller cameras than the A-3
Single-seat night fighter aircraft, later night and bad weather fighter with enlarged wing and DB603L engines.
Two-seat night fighter aircraft, with completely separate second cockpit located above and behind the original.
A-6 with longer wing.
A-4 fitted with longer wing.
A-4 fitted with longer wing, DB603L engines and pressurized cockpit.
Proposed night fighter trainer.
Two seat trainer. A second cockpit was mounted behind and above the front cockpit.
Abandoned in development.
Single-seat destroyer aircraft. Fitted with 2 additional MK 103 in the wings and provision to carry two standard Luftwaffe 300 litre drop tanks.
Updated B-1 but with longer wing.
Update of the B-1 with longer wing, DB603L engine.
Night fighter. Two DB 603E engines.
High altitude night fighter. Two DB 603LA engines.
High altitude night figther. Larger wing area.
Dual-seat trainer version for the B-series aircraft.
Design that had more powerful engines and larger fuselage.
Design that had twin fuselages with a central section inbetween. Was to have four engines.


7400 kg
9610 kg
11700 kg
13.85 m
13.8 m
38.5 m²
4.55 m
192.208 - 249.351 kg/m²

1 × 30 mm (1.18 in) MK 103 cannon
2 × 30 mm (1.18 in) MK 103 cannon *
2 x 70
2 × 20 mm MG 151/20
Up to 1000 kg bombload (Internal Bay)

(*) on Do-335B-2 model

2 × Daimler-Benz DB 603A
liquid-cooled inverted V12, 44.52 L
2 x 1726 hp
359 hp / ton *
1930 L

(*) with loaded weight

765 km/h at 6400 m
475 km/h at 6000 m
? km/h
11400 m
8,88 m/s
1390 km, 2060 km / 3750 km °°

(*) vitesse de décrochage, (**) external fuel