Technical data
Type KOR-1
Function reconnaissance
Year 1936
Crew 2
Engines 1*635/700hp M-25
Length 8.67m
Height ?m
Wingspan 11.0m
Wing area 29.3m2
Empty weight 1800kg
Loaded weight (normal) 2486kg
Loaded weight (overload) 2686kg
Wing Load (kg/m2) 85(92)
Power load (kg/hp) 3.6(3.8)
Speed at 0m 245km/h
Speed at 2000m 277km/h
Landing Speed 100km/h
Landing Roll 16sec
Takeoff Roll 250m 15sec
Turn time 18sec
Range 530(1000)km
Flight Endurance 3hmin
Ceiling 6600m
Climb
1000m 3.2min
5000m 20min
Payload
Fuel 293kg
Armament
Guns 2+1*7.62mm ShKAS
Bombs (overload) 2*100kg FAB-100

KOR-1 (KR-2, TsKBMS-3), G.M.Beriev (NATO 'Mote')

29k photo of the KOR-1, courtesy of

License-built KR-1 flying boat turned obsolete in mid-30's, and in 1934 first records appear about next generation reconnaissater (designated KR-2). It was intended for catapult launch from 'Kirov' class cruisers. Ice-breaking fleet of the Polar seas also was interested.

KR-2 project was assigned to the Taganrog-based TsKBMS, lead by G.M.Beriev. On 22 November 1934 the VVS Command approved project of classic single-float biplane, designated KOR-1 (TsKBMS-3).

(32k) KOR-1 model; posted this photo in November 1996 on his Page;

New aircraft had to fulfill following duties:

Created November 25, 1996
Modified June 16, 1999
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