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OVERVIEW
RIKUGUN Ki-202 SYUSHUI-KAI
1946
 
FIGHTER/INTERCEPTOR - PROJECT
 
     
 
 
OVERVIEW
 
 

More to come

 
     
 
DATA
 
 
RIKUGUN Ki-202 SYUSHUI-KAI
 (PERFORMANCE DATA ESTIMATED)
CLASSIFICATION
CLASS :
 FIGHTER/INTERCEPTOR - PROJECT
COUNTRY OF ORIGIN :
 IMPERIAL JAPAN
MANUFACTURER :
 RIKUGUN KOKU GIJUSTO KENKYUJO - ARMY AEROTECHNICAL
 
 RESEARCH INSTITUTE
FIRST FLIGHT :
 PLANNED FOR 1946
SERVICE DELIVERY :
 NONE
NUMBER BUILT :
 0
   
SPECIFICATION
SPAN :
 31.9 ft (9.72 m)
LENGTH :
 25.2 ft (7.68 m)
HEIGHT :
 9 ft (2.74 m)
WING AREA :
 198 sq ft (18.39 m sq)
WEIGHT EMPTY :
 3,569 lbs (1619 kg)
WEIGHT LOADED :
 7,460 lbs (3384 kg)
WEIGHT MAX :
 11,057 lbs (5015 kg)
ARMAMENT :
 2 x 30mm Ho-155 Cannons
BOMB LOAD :
 --
POWER PLANT :
 1 x Toku-Ro (KR20) Bi-Fuel Rocket Motor Engine, Producing 4,409 lbs
 
 (2,000 kg) & 1 x Supplementary Rocket or Cruise Chamber, Producing
 
 880 lbs (400 kg) of Thrust
CREW :
 1
 
 
PERFORMANCE
MAXIMUM SPEED :
 559 mph (900 km/h) at 32,808 ft (10000 m)
CRUISING SPEED :
 --
LANDING SPEED :
 82 mph (132 km/h)
CLIMB RATE :
 To 6,561 ft (2000 m) in 1 min 21 sec
 
 To 13,123 ft (4000 m) in 2 min 0 sec
 
 To 19,685 ft (6000 m) in 2 min 34 sec
 
 To 26,246 ft (8000 m) in 3 min 2 sec
 
 To 32,808 ft (10000 m) in 3 min 26 sec
RANGE :
 Endurance of 10 min 28 sec
SERVICE CEILING :
 39,370 ft (12000 m)
 
 
 
 
REFERENCES
 
 

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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