Overview
Introduced in early 1917, the LFG Roland D.II biplane fighter saw production reach 300 units before the end of World War 1.
Introduced in early 1917, the LFG Roland D.II biplane fighter saw production reach 300 units before the end of World War 1.
History
Detailing the development and operational history of the LFG Roland D.II (Shark) Single-Seat Biplane Fighter Aircraft. Entry last updated on 7/31/2019. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
Detailing the development and operational history of the LFG Roland D.II (Shark) Single-Seat Biplane Fighter Aircraft. Entry last updated on 7/31/2019. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
LFG Roland of Germany built a healthy, deep stable of combat aircraft for the German Empire during World War 1 (1914-1918) and this included fixed-wing types as well as airships. A development of 1916 became the D.II - later known as the "Shark" - a single-seat, single-engine biplane fighter that was adopted for service in early-1917 and produced to the tune of 300 examples by both LFG Roland and competitor Pfalz. The D.II was developed from the earlier D.I biplane which, itself, was a further evolution of the two-seat C.II reconnaissance mount. The D.II was fielded by the German Empire and Bulgarian air services.
Due to its origins in the C.II/D.I, the D.II carried over similar physical features that included a streamlined, and rather deep, fuselage. A large spinner covered the propeller hub. The biplane wing arrangement showcased single bays with parallel strut works and applicable cabling. The pilot sat aft and under the upper wing assembly - though the wing itself sat low over the forward fuselage and restricted much of the forward-down, forward-side vision from the pilot. A wheeled, tail-dragger undercarriage was featured as was a single vertical tail fin.
Internally, the D.II was completed with a plywood monocoque fuselage construction. The fuselage was essentially made up of two halves joined at a center line (with glue) and the entire structure was skinned over in fabric for added strength. Not only did this provide for the needed clean and aerodynamically refined look of the aircraft it also produced a rather lightweight overall structure.
Armament was conventional for the period - 2 x LMG08/15 (Spandau) series machine guns set over the nose and synchronized to fire through the spinning propeller blades by way of "interrupter" gear.
As finalized, the D.II design could stay aloft up to two hours and reach a ceiling of over 16,000 feet. Maximum speed was listed at 112 miles per hour.
The initial field variant was known simply as "D.II" and these forms carried the Mercedes D.III piston engine of 160 horsepower. The mark was followed by the "D.IIa" which switched over to an Argus As.III engine of 180 horsepower but, despite the added output power, the aircraft suffered at altitudes beyond 10,000 feet - forcing the type to low-level operations. The C.V existed as a "one-off" two-seat prototype form still carrying the original Mercedes D.III engine (160 horsepower). Pfalz-produced D.II and D.IIa models were designated as D.II (Pfal) and D.IIa (Pfal) respectively to differentiate their factory origins. One hundred of each form were produced by Pfalz Flugzeugwerke.
In service, the aircraft did not prove itself as formidable as its appearance would suggest. Controlling was deemed below average, requiring a steady hand by the pilot and some useful experience in combat, and vision out-of-the-cockpit was poor owing to the placement of the upper wing assembly. Where the D.II did shine was in straightline performance from its Mercedes engine coupled with the sleek fuselage - it could match or outpace contemporary fighters. It was also well-armed and featured a strong internal structure.
Due to its origins in the C.II/D.I, the D.II carried over similar physical features that included a streamlined, and rather deep, fuselage. A large spinner covered the propeller hub. The biplane wing arrangement showcased single bays with parallel strut works and applicable cabling. The pilot sat aft and under the upper wing assembly - though the wing itself sat low over the forward fuselage and restricted much of the forward-down, forward-side vision from the pilot. A wheeled, tail-dragger undercarriage was featured as was a single vertical tail fin.
Internally, the D.II was completed with a plywood monocoque fuselage construction. The fuselage was essentially made up of two halves joined at a center line (with glue) and the entire structure was skinned over in fabric for added strength. Not only did this provide for the needed clean and aerodynamically refined look of the aircraft it also produced a rather lightweight overall structure.
Armament was conventional for the period - 2 x LMG08/15 (Spandau) series machine guns set over the nose and synchronized to fire through the spinning propeller blades by way of "interrupter" gear.
As finalized, the D.II design could stay aloft up to two hours and reach a ceiling of over 16,000 feet. Maximum speed was listed at 112 miles per hour.
The initial field variant was known simply as "D.II" and these forms carried the Mercedes D.III piston engine of 160 horsepower. The mark was followed by the "D.IIa" which switched over to an Argus As.III engine of 180 horsepower but, despite the added output power, the aircraft suffered at altitudes beyond 10,000 feet - forcing the type to low-level operations. The C.V existed as a "one-off" two-seat prototype form still carrying the original Mercedes D.III engine (160 horsepower). Pfalz-produced D.II and D.IIa models were designated as D.II (Pfal) and D.IIa (Pfal) respectively to differentiate their factory origins. One hundred of each form were produced by Pfalz Flugzeugwerke.
In service, the aircraft did not prove itself as formidable as its appearance would suggest. Controlling was deemed below average, requiring a steady hand by the pilot and some useful experience in combat, and vision out-of-the-cockpit was poor owing to the placement of the upper wing assembly. Where the D.II did shine was in straightline performance from its Mercedes engine coupled with the sleek fuselage - it could match or outpace contemporary fighters. It was also well-armed and featured a strong internal structure.
Specifications
YEAR: 1917
STATUS: Retired, Out-of-Service
MANUFACTURER(S): Luft-Fahrzeug-Gesellschaft GmbH (LFG Roland) / Pfalz - Imperial Germany
PRODUCTION: 300
CREW: 1
LENGTH: 22.80 ft (6.95 m)
WIDTH: 29.36 ft (8.95 m)
HEIGHT: 10.24 ft (3.12 m)
EMPTY WEIGHT: 1,576 lb (715 kg)
MTOW: 2,105 lb (955 kg)
POWER: 1 x Mercedes D.III 6-cylinder in-line water-cooled piston engine developing 160 horsepower and driving two-bladed wooden propeller in nose.
SPEED: 112 mph (180 kph; 97 kts)
CEILING: 16,404 feet (5,000 m; 3.11 miles)
RANGE: 224 miles (360 km; 194 nm)
RATE-OF-CLIMB: 715 ft/min (218 m/min)
OPERATORS: Bulgaria; German Empire
Armament
2 x 7.92mm LMG08/15 machine guns over nose synchronized to fire through the spinning propeller blades.
2 x 7.92mm LMG08/15 machine guns over nose synchronized to fire through the spinning propeller blades.
Variants / Models
• D.II - Base Series Designation; initial production model; fitted with Mercedes D.III piston engine of 160 horsepower.
• D.IIa - Fitted with Argus As.III series engines of 180 horsepower.
• C.V - Single two-seat prototype; fitted with Mercedes D.III engine of 160 horsepower.
• D.II (Pfal) - Production of D.II aircraft by Pfalz
• D.IIa (Pfal) - Production of D.IIa aircraft by Pfalz
• D.II - Base Series Designation; initial production model; fitted with Mercedes D.III piston engine of 160 horsepower.
• D.IIa - Fitted with Argus As.III series engines of 180 horsepower.
• C.V - Single two-seat prototype; fitted with Mercedes D.III engine of 160 horsepower.
• D.II (Pfal) - Production of D.II aircraft by Pfalz
• D.IIa (Pfal) - Production of D.IIa aircraft by Pfalz
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed
Hi: 120mph
Lo: 60mph
This entry's maximum listed speed (112mph).
Graph average of 90 miles-per-hour.
City-to-City Ranges
NYC
LDN
LDN
PAR
PAR
BER
BER
MSK
MSK
TKY
TKY
SYD
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LAX
LAX
NYC
Graph showcases the LFG Roland D.II's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production (300)
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
300
300
Altitude Visualization
