Flat 36 Vias Roland Sp300v
Contents.Design and development Just before the term Pfeilflieger was used to describe a category of with swept back wings, a feature adopted to provide some automatic stability. At least six other manufacturers (, and ) as well as LFG designed and built them, though some had less sweep than others. Most had Pfeilflieger in their name.The LFG Arrow was amongst the more strongly swept of the class. It had wings of unequal span, with only on the overhung upper planes. There was marked on the lower wing but none on the upper. With three pairs of long on each side, the LFG was a with a large interplane gap. It could be powered either by a 100 hp (75 kW) water cooled six cylinder inline engine or by a four-cylinder inline engine of the same output.
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The Argus engined version had a span reduced by 0.69 m (2 ft 3 in), 81% of the wing area and a slightly longer fuselage.The was flat sided and rectangular in section, with the engine exposed in the nose and the passenger/observer's immediately behind it. In some engine installations the was mounted along the fuselage side, with this cockpit between them.
The pilot's cockpit, fitted like the passenger's with a, was much further aft at about mid-fuselage with the main fuel tank between them. Because the LFG had a very broad, low horizontal tail of the sort known at the time as 'Taube type', he sat not far in front of the its. The tailplane carried an undivided.
There was a triangular and a high, rounded. The Arrow had a fixed, with V-form struts, their leading members bent round into short skids laterally connected by a rod to which the wheels, on their single axle, were joined via rubber. A Roland Pfeilflieger used by the in German South-West AfricaBefore the outbreak of Bernard Langer flew a Roland Pfeilflieger, equipped with a Mercedes engine and extra tankage in place of the passenger, on a non-stop sixteen-hour flight. During the war at least one LFG Roland Pfeilflieger served with the (Protection Force) in German South-West Africa, now between 1914 and 1915. Variants Mercedes D.I engine as described Argus As I engine span 12.34 m (40 ft 6 in); length 8.08 m (26 ft 6 in); wing area 32.5 m 2 (350 sq ft) Specifications (with Mercedes D.I engine). The smaller span, Argus powered PfeilfliegerData from Flight 1 August 1914, p.877General characteristics.
Crew: Two. Length: 8.00 m (26 ft 3 in).
Upper wingspan: 12.95 m (42 ft 6 in). Height: 3.30 m (10 ft 10 in). Wing area: 40 m 2 (430 sq ft). Empty weight: 626 kg (1,380 lb).
Gross weight: 975 kg (2,150 lb). Powerplant: 1 × water cooled inline, 75 kW (100 hp). Propellers: 2-bladedPerformance. Maximum speed: 100 km/h; 54 kn (62 mph). Combat range: 499 km; 269 nmi (310 mi). Endurance: 5 hours with standard tanksReferences.
Contents.Design and development The V 59 and V 61 were both twin float seaplanes, essentially identical apart from their engines and designed to carry four or five passengers. The V 59 was powered by a 240 hp (179 kW) 6-cylinder water cooled inline and the V 61 by a much more powerful, 400 hp (298 kW) 9-cylinder radial. They were metal aircraft both in frame and covering, of the semi- kind with external bracing between the upper and wing and further support from below via the flat topped floats. The wings were straight tapered with rounded. The fuselage was flat sided and bottomed, with windows down the side and with a braced mounted on top of it.
The rudder extended well below the keel. The LFG V 61 (foreground) and V 60 (right) at the 1926 German Seaplane Competition Operational history Both the V 59 and the V 61 were entered into the German Seaplane Competition, held between 12–23 July 1926 with flights along the and coasts from. The V 59 did not score in the technical tests but the V 61 came sixth in them whilst not completing the whole course. Variants V 59 240 hp (179 kW) 6-cylinder water cooled inline engine. Four passengers. V 61 400 hp (298 kW) 9-cylinder.
Estimated maximum speed 185 km/h (115 mph). Five passengers.
Flat 36 Vias Roland Sp300v 1
Specifications (V 59) Data from Flight 22 July 1926 pp.448-451General characteristics. Crew: 2. Capacity: 4/5 passengers. Wing area: 52 m 2 (560 sq ft). Empty weight: 1,430 kg (3,153 lb). Gross weight: 2,200 kg (4,850 lb).
Powerplant: 1 × 6-cylinder inline water cooled, 180 kW (240 hp)Performance. Maximum speed: 151 km/h (94 mph; 82 kn)References Wikimedia Commons has media related to.