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OVERVIEW
NAKAJIMA Ki-201 KARYU
1946
 
FIGHTER/BOMBER PROJECT
  
 
 
DATA
  
 
NAKAJIMA Ki-201 KARYU
 
CLASSIFICATION
CLASS :
 FIGHTER - PROJECT
COUNTRY OF ORIGIN :
 IMPERIAL JAPAN
MANUFACTURER :
 NAKAJIMA HIKOKI KABUSHIKI KAISHA (Nakajima Aircraft Company, Ltd)
FIRST FLIGHT :
 1946
SERVICE DELIVERY :
 NONE
NUMBER BUILT :
 0
   
SPECIFICATION
SPAN :
 44.9 ft (13.68 m)
LENGTH :
 37.7 ft (11.49 m)
HEIGHT :
 13.3 ft (4.05 m)
WING AREA :
 258 sq ft (23.96 m)
WEIGHT EMPTY :
 9,910 lbs (4495 kg)
WEIGHT LOADED :
 15,478 lbs (7021 kg)
WEIGHT MAX :
 18,722 lbs (8492 kg)
POWER PLANT :
 2 x Ishikawajima Ne-230 Axial-Flow Turbojet Engines, Producing
 
 1,951 lbs (885 kg) of Thrust ea. or
 
 2 x Ishikawajima Ne-130 Axial-Flow Turbojet Engines, Producing
 
 2,002 lbs (908 kg) of Thrust ea.
ARMAMENT :
 2 x 30mm Ho-155 Cannons and 2 x 20mm H0-5 Cannons in Nose
BOMB LOAD :
 1 x 1,102 lb (500 kg) or 1 x 1,764 lb (800 kg) Bombs
CREW :
 1 - Pilot
   
PERFORMANCE
MAXIMUM SPEED :
 (w/ Ne-230) 504 mph (812 km/h) at 32,808 ft (10000 m)
 
 (w/ Ne-130) 525 mph (845 km/h) at 32,808 ft (10000 m)
CRUISING SPEED :
 
LANDING SPEED :
 100 mph (161 km/h)
CLIMB RATE :
 (w/ Ne-230) To 19,685 ft (6000 m) in 6 min 54 sec
 
                   To 32,808 ft (10000 m) in 14 min 56 sec
 
 (w/ Ne-130) To 19,685 ft (6000 m) in 6 min 17 sec
 
                   To 32,808 ft (10000 m) in 13 min 15 sec
RANGE :
 613 miles (987 km) at 26,230 ft (7995 m)
SERVICE CEILING :
 39,370 ft (12000)
 
 
 
 
 
 
REFERENCES
  
 

Green, William; Swanborough, Gordon. The Complete Book of Fighters. New York: Barnes & Noble Books. 1998. ISBN 0-07607-0904-1.

Dyer, Edwin M., Japanese Secret Projects - Experimental Aircraft of The IJA and IJN 1939-1945. UK:Ian Allan Publishing . 2009. ISBN 978-1857803-174.

  
 
     
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