History of Dornier Do p. 254 (Do 535 / He 535)

The Dornier Do P. 254 project existed as a short-lived outgrowth of the Do 335 "Pfeil" ("Arrow") heavy fighter project. On the Do 335, one engine is attached to the nose of the aircraft in the usual fashion (a "pull-rod" arrangement), but the rear of the fuselage also makes room for the transport of a second engine, which runs in a "push-hand". arrange. Combined engines made the Do 335 the fastest propeller-driven aircraft introduced from Germany during World War II.

However, before the end of the war in 1945, engine delays resulted in limited instances of operation, with only about 37 delivered. The aircraft program was also overshadowed by the Focke-Wulf Ta 152 high-altitude fighter.

The P. 254 (Do 535) was designed to benefit from the foundation laid by the Do 335 by retaining the nose-mounted Daimler-Benz DB603A piston engine but replacing the rear-wheel drive system with a Heinkel-Hirth HeS 011 replaced Turbojet, which adds 2,866 pounds of thrust. In theory, the P. 254 would be a faster propeller-driven system than the Do 335, but it lacked the swept wings that favored high-speed flight.

With the Luftwaffe's preference for the more traditional, competitive Ta 152 high-altitude fighter, DORNIER engineers hope to add jet engines to their Do 335, which will keep this promising heavy fighter program alive for some time.

It is unclear what role the P. 254 played on the battlefield to accomplish combat missions, but it may have been similar to postwar Germany's usual push for viable fighters, interceptors and night fighters that had to withstand day and night bombing raids by the Allies. Most likely, a secondary role for high-speed bombs should be built.

Despite the adventure, no P. 254 aircraft were built to the existing Do 335 design, and the plan was ultimately not seriously considered - but before it was passed to Heinkel and redrafted as He 535 in October 1944 . [ /p]

Specification

Basic

Year:
1945
Staff:
1

Production

[0 units]:
Dornier Flugzeugwerke / Heinkel - Nazi Germany

Roles

- Fighter

- Ground Attack

- X-Plane / Development

Dimensions

Length:

45.44 ft (13.85 m)

Width:

45.28 ft (13.8 m)

Height:

14.93 ft (4.55 m)

Weight

Curb Weight:

7,600 kg

MTOW:

10,100 kg

(difference: +5,512 pt)

Performance

1 x Daimler-Benz DB603A 12-cylinder reversible engine producing 1,725 ??hp and driving a three-bladed propeller in the nose; 1 x Heinkel-Hirth HeS 011 turbojet in the aft fuselage, 2,866 lbs of thrust.

Performance

Maximum Speed:

525 mph (845 km/h; 456 knots)

Service Limit:

40,026 ft (12,200 m; 7.58 mi)

Maximum range:

932 miles (1,500 km; 810 nautical miles)

Rate of climb:

701 m/min (2,300 ft/min)

Armor

Accept (based on Do 335):

1 x 30mm MK 103 gun firing through the nose of the propeller hub.

2 x 20 mm MG 151/20 cannons in the fairing, fired synchronously by rotating propeller blades.

Optional:

Up to ?2,200 in externally held outlet stores.

Changes

page 254 - Base item names

Do 535 - Alternative Project Names

He 535 - Modified name

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