torstai 24. maaliskuuta 2016

Shchetinin M-5 Stetinin

Grigorovich M-5 (alternative designation Shch M-5, sometimes also Shchetinin M-5) was a successful Russian World War I-era two-bay unequal-span biplane flying boat with a single step hull, designed by Grigorovich. It was the first mass production flying boat built in Russia.
The aircraft designer Dmitry Pavlovich Grigorovich completed his first flying boat (the model M-1) in late 1913, and produced a series of prototypes, gradually improving the design, until the M-5 appeared in the spring of 1915, which was to be his first aircraft to enter series production, with at least 100 being produced, primarily to replace foreign built aircraft, including Curtiss Model K and FBA flying boats.
The M-5 was of a wooden construction, the hull was covered in plywood and the wings and tailplane were covered in fabric. Aft of the step the hull tapered sharply into little more than a boom, supporting a characteristic single fin and rudder tail unit, which was braced by means of struts and wires. It was normally powered by a 100 hp Gnome Monosoupape engine mounted as a pusher between the wings, but some used 110 hp Le Rhône or 130 hp Clerget engines. The pilot and the observer were accommodated side-by-side in a large cockpit forward of the wings, the observer provided with a single 7.62 mm Vickers machine gun on a pivoted mounting.
Most of the M-5s served in the Black Sea or in the Baltic, initially with the Imperial Russian naval air arm and later with both sides in the Russian Civil War. Some remained in service until the late 1920s as trainers, reconnaissance and utility aircraft.
One M-5 fell into Finnish hands when it was found drifting at Kuokkala in 1918. The aircraft was flown by the Finnish Air Force until 1919, when it sank.
- Finnish Air Force
- Imperial Russian Navy
- White Army
- Russian SFSR
- Red Army
- Soviet Union
- Soviet Naval Aviation
Specifications M-5
Crew: 2
Length: 8.6 m 
Wingspan: 13.62 m 
Wing area: 37.9 m2 
Empty weight: 660 kg 
Max takeoff weight: 960 kg
Powerplant: 1 × Gnome Monosoupape 9 Type B-2 9-cyl. air-cooled rotary piston engine, 75 kW 101 hp
Maximum speed: 105 km/h 
Endurance: 4 hours
Service ceiling: 3,300 m 
Rate of climb: 1.85 m/s 
Time to altitude: 1,000 m in 9.6 minutes
Wing loading: 25 kg/m2 
Power/mass: 0.078 kW/kg 

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