Search filter

    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      13 m
      20 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      7800 kg
      11700 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      211 km/h
      318 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      2880 hp
      4320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4632 m
      6948 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      467 km
      701 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      2 qt
    • Bombs
      1 qt
      2 qt
    • Missiles
      1 qt
      2 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      3 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      142 qt
      214 qt
    • Price
      41 USD
      750000000 USD

Mitsubishi H-60

TypeHelicopter
Company

Mitsubishi Aircraft Corporation

Geometry
Length (m)
1.9
 
19.8
88.7
Height (m)
0.6
 
5.2
50.1
Rotors
Main rotor diameter (m)
1.2
 
16.4
62
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
9,750
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
264.8
28,165
Power
Total Power (hp)
0.4
 
3,600
60,000
2 powerplants 1800 hp each
Performance
Service ceiling (m)
0.6
 
5,790
161,544
Range (Ferry range) (km)
4
 
584
40,700
Combat
Guns (qt)
1
 
1
18
7.62 mm (.30 in) Type 74 machine gun
Bombs (qt)
1
 
1
250
Depth charge
Missiles (qt)
1
 
1
24
AGM-114 Hellfire
Torpedoes (qt)
1
 
4
4
2 x Mark 46 torpedo; 1 x Type 74 torpedo; 1 x Type 12 torpedo
Stat
Number built (qt)
0
 
178
43,000
First flight 31.08.1987

Similar aircraft

Get more

Comments