Technical data
Type '104'
Function Interceptor
Year 1944
Crew 4?
Engines 2*1460/1850hp ASh-82FN
Length 13.8m
Wingspan 18.86m
Wing area 48.8m2
Empty weight 7474kg
Loaded weight (no bombs) 10360kg
Loaded weight 11360kg
Wing Load (kg/m2) 211
234
Power load (kg/hp) 3.0
3.3
Speed at 0m 482km/h
Speed at 0m (boosted) 509km/h
Speed at 2400m 530km/h
Speed at 5400m 547km/h
Landing Roll 675m
Takeoff Roll 485m
Turn time ?sec
Range 2100km (with 1500kg bombs)
Ceiling 9500m
Climb
5000m 9.5min
Armament
Guns 3 defensive 12.3mm UBT
2*20mm 'ShVAK' in the wing roots
2*23mm 'VYa-23' in the nose

'104' by A.N.Tupolev/ STO-3/ OTB


Series Tu-2S modified for interceptor role. It carried aiming radar (A.L.Mints) and two additional VYa-23 cannons in the nose.

First flight (pilot A.D.Perelet, engineer L.L.Kreber) took place on July 18, 1944. Flight characteristic were not better than for standard Tu-2S, and aircraft '104' development was cancelled. Aircraft was used in 1944- 1945 for experiments with aiming radar for fighters.

The only '104' aircraft was rebuilt as UTB in February 1946.

PredecessorsModifications

Tu-2S 61 ANT-61
UTB

ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.179;
  • ...

  • Created on August 17, 1998 Back to
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