|First flight||October 1916|
|Developed from||Roland D.I|
Design and development[edit | edit source]
The D.II used a plywood monocoque fuselage. Two layers of plywood strips were spirally wrapped in opposing directions over a mold to form one half of a fuselage shell. The fuselage halves were then glued together, covered with a layer of fabric, and doped. The upper wing was attached to the fuselage by means of a large central pylon, greatly impairing the pilot's forward vision. Armament consisted of twin "Spandau" LMG 08/15 machine guns buried in the fuselage decking.
The D.II was initially powered by a 160 hp Mercedes D.III engine, giving a top speed of 105 mph at sea level. Later aircraft, designated D.IIa, were powered by an 180 hp Argus As.III. The As.III offered poor performance above 3,000 m and the D.IIa was mostly relegated to operations on the Eastern Front.
Nicknamed Haifisch (shark) for its sleek appearance, the D.II and D.IIa proved generally unpopular in service due to poor fields of view and heavy controls. However, it is also reported that the aircraft had particularly sensitive controls, particularly in the yawing plane. The type is known to have been used by Jasta 25 at their Canatlarzi base in Macedonia in 1917.
Variants[edit | edit source]
- D.II: Single-seat fighter-scout biplane, powered by a 160 hp (119 kW) Mercedes D.III piston engine.
- D.IIa: Single-seat fighter-scout biplane, powered by a 180 hp (134 kW) Argus As.III piston engine.
- C.V: One-off two seat derivative with a 160 hp (119 kW) Mercedes D.III engine.
Operators[edit | edit source]
Specifications (D.II)[edit | edit source]
Data from German Aircraft of the First World War 
- Crew: 1
- Length: 6.93 m (22 ft 8⅞ in)
- Wingspan: 8.94 m (29 ft 4 in)
- Height: 3.11 m (10 ft 2⅜ in)
- Wing area: 22.8 m² (246.2 ft²)
- Empty weight: 715 kg (1,573 lb)
- Loaded weight: 954 kg (2,099 lb)
- Powerplant: 1 × Mercedes D.III 6-cylinder in-line water-cooled piston engine, 119 kW (160 hp)
- Maximum speed: 180 km/h (97 knots, 112 mph)
- Service ceiling: 5,000 m  (16,400 ft)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: W/kg (hp/lb)
- Climb to 5,000 m (16,400 ft): 23 min
- Endurance: 2 hours 
See also[edit | edit source]
- LFG Roland C.II
- LFG Roland D.I
- LFG Roland D.III
- Pfalz D.III
- Albatros D.II
- Albatros D.III
- Siemens-Schuckert D.I
- Nieuport 17
- Spad VII
- Airco DH-2
- Sopwith Pup
- List of military aircraft of Germany
References[edit | edit source]
|Wikimedia Commons has media related to Roland D.II.|
- Cowin, H. W. "German and Austrian Aviation of World War I". Osprey Publishing Ltd, 2000. ISBN 1-84176-069-2
- Gray and Thetford 1962, p.164-165.
- Angelucci 1981, p.50.
- Donald 1994, p. 554.
- Angelucci, Enzo (editor). World Encyclopedia of Military Aircraft. London:Jane's, 1981. ISBN 0-7106-0148-4.
- Donald, David (editor). The Encyclopedia of World Aircraft. London:Blitz, 1997. ISBN 1-85605-375-X.
- Gray, Peter and Thetford, Owen. German Aircraft of the First World War. London: Putnam, 1962.
- Green, William and Swanborough, Gordon. The Complete Book of Fighters. London: Salamander Books, 1994. ISBN 0-8317-3939-8.
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