Slesarev Svyatogor

Slesarev Svyatogor

infobox Aircraft
name = Svyatogor
type = Experimental bomber
logo =
manufacturer =


300px
caption = Svyatogor
designer = V.A.Slesarev
first flight =
introduction =
retired =
status =
primary user =
more users =
produced =
number built =
unit cost =
developed from =
variants with their own articles =
The Svyatogor ( _ru. Святогор) was a large experimental Russian aircraft, constructed by V.A.Slesarev in 1916. The aircraft was named after the mythological hero Svyatogor.

Development

The work on the Svyatogor began in 1913. It was a large wooden biplane, with wings and fuselage covered in fabric. The aircraft was propelled by two large propellers, 6 meters in diameter. Everything on the aircraft was over-sized, the nose wheel was 1.5 meter in diameter and the four rear wheels were 2 meters in diameter. The engines were placed inside the fuselage to allow accuss during flight.

The aircraft awoke much interest, but failed to receive funding before WWI. In desperate need of aircraft, the project was given a 100,000 rubles funding by E.M.Malynsky and production started in December 1914.

As suitable engines were hard to come by, Slesare tried to mount some that had been taken from a downed Zeppelin. He contacted the French when this didn't work out, and received some Renault engines, which could produce 220 horsepowers. These arrived in January 1916. Despite being without money, the construction of the revised design continued. The project stalled however with the transmission problems and the death of Slesarev in 1921.

pecifications

aircraft specifications

plane or copter?=plane
jet or prop?=prop

ref=

crew=3
capacity=
payload main=
payload alt=
length main= 21.0 m
length alt=68 ft 11 in
span main= 36.0 m
span alt=118 ft 1 in
height main=
height alt=
area main= 180 m²
area alt= 1,938 ft²
airfoil=
empty weight main= 3,200 kg
empty weight alt=7,055 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 6,500 kg
max takeoff weight alt= 14,330 lb
more general=

engine (prop)=Renault
type of prop=
number of props=2
power main= 149 kW
power alt=200 hp
power original=

propeller or rotor?=
propellers=
number of propellers per engine=
propeller diameter main=
propeller diameter alt=

max speed main= 100 km/h
max speed alt= 62 mph, 54 knots
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=
range alt= 30 h
ceiling main= 2,500 m
ceiling alt= 8,200 ft
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=

armament=
guns=
bombs=
rockets=
missiles=
hardpoints=
hardpoint capacity=

avionics=


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