川崎: KH-4
Kawasaki: KH-4

General data

Producer info

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Names and dates
Market original model designation
KH-4
Market model designation (english translation or spelling)
KH-4
First flight date and time
1962
Production start date
1962
Production end date
1975
Country of manufacture
Japan
Config info
Rotorcraft typeHelicopter
Weights
Maximum Takeoff Weight (MTOW)
1293
kg
Manufacturers empty weight (MEW)
816
kg
Cabin and cockpit
Maximum number of people onboard
4
External dimensions
Fuselage length
9.93
m
Height
2.84
m
Total length (rotors turning)
13.30
m
Main rotor
Main rotor diameter
11
m
Number of blades
2
Tail rotor
Tail rotor diameter
1
m
Number of blades
2
Powerplant
Engine model
Lycoming TVO-435-B1A
Engine type
Piston
Number of engines
1
Total maximum power
270
HP
Performance
Never exceed speed (Vne)
169
km/h
Max cruise speed
141
km/h
Maximum service ceiling
5640
m
Maximum range
400
km
0.0904