Technical data
Type Tu-2-2ASh-83
Function Bomber
Year 1945
Crew 4
Engines 2*1900hp ASh-83
Length 13.8m
Wingspan 18.86m
Wing area 48.8m2
Empty weight 7685kg
Loaded weight (no bombs) 10585kg
Loaded weight 11575kg
Wing Load (kg/m2) 217kg/m2
237
Power load (kg/hp) 2.8kg/hp
3.1
Speed at 0m 528km/h
Speed at 0m (boosted) 509km/h
Speed at 6800m 605km/h
Landing Speed 160km/h
Takeoff Roll 480m
Range 1950km
Ceiling 10400m
Climb
5000m 8.5min
Armament
Guns 3 defensive 12.3mm UBT
2*20mm ShVAK in the wing roots
Bombs 1000kg inside
plus up to 3000kg externally (overload)

Tu-2-2ASh-83 by A.N.Tupolev


A Tu-2S variant (Number 100716) with 1900hp high-altitude engine. Aircraft was built in 1945, substantial increase in speed came on expense of minor range loss.

PredecessorsModifications

'61' Tu-2S ANT-61
None?

ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.175;
  • None found.

  • Created on August 13, 1998 Back to
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