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Arado Ar 81

The Arado Ar 81 was a German prototype dive bomber.

The Ar 81 was built as an all metal biplane.

It was a pleasant design, which looked rather more streamlined than the first prototype of the Ju 87, and was slightly smaller and lighter.

The slender fuselage had a closely cowled Junkers Jumo 210C engine in front, with a large radiator bath below it.

The wings were relatively short in span and connected by N-struts outboard.

Behind the wings, the crew of two sat in a roomy cockpit with a semi enclosed canopy, back to back.

The rear of the cockpit canopy was open to allow the gunner to freely aim his defensive machine gun.

The fixed main landing gear legs were fitted with streamlined covers and spats for the wheels.

The tail section was very slender, and the tail of the first prototype, Ar 81V1, consisted of a tailplane with some dihedral that carried two outboard fins and rudders, to improve the field of fire of the tail gunner.

However, testing from the end of 1935 onward revealed serious stability problems.

The second prototype was given a raised tailplane without dihedral, braced with struts, but this did not cure the issues, and the third prototype had a completely reworked tail, with a boom structure of larger cross-section that carried a tall single tailfin and a large rudder.

This prototype also had a Jumo 210Ca engine that drove a two bladed variable pitch propeller, instead of the three-bladed fixed-pitch unit fitted to the first two prototypes.

The defensive armament of a single fixed MG 17 machine gun, intended to be fitted in the engine cowling, and a MG 15 defensive gun in the rear cockpit, was probably never installed.

The same is claimed for the special bomb rack below the fuselage, intended to swing a 250 kg bomb clear of the propeller in a diving attack. 

However, test pilot Kurt Starck claimed that during the 1936 trials, the Ar 81 was the only aircraft capable of dropping a 500 kg bomb in a vertical dive, which indicates that a bomb rack must have been fitted.





11.65 m (38 ft 3 in)


11.2 m (36 ft 9 in)


3.57 m (11 ft 9 in)

Wing area

35.6 m2 (383 sq ft)

Empty weight

1,925 kg (4,244 lb)

Gross weight

3,070 kg (6,768 lb)


1 × Junkers Jumo 210Ca, inverted V-12 liquid cooled piston engine,

480 kW (640 hp) at 2,700 m (8,900 ft)


2 bladed variable pitch propeller


Maximum speed

345 km/h (214 mph, 186 kn) at 4,000 m (13,000 ft)


693 km (431 mi, 374 nmi) at 4,000 m (13,000 ft)

Service ceiling

7,698 m (25,256 ft)

Time to altitude

At 4,000 m (13,000 ft) in 11 minutes



1 × 7.92 mm (0.312 in) MG 17 machine gun fixed in the engine cowling,

1 × 7.92 mm (0.312 in) MG 15 machine gun flexible in the rear cockpit


1 × 250 kg (550 lb) bomb on a swinging crutch under the fuselage.


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