Search filter

    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      5 m
      9 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
      17 m
      27 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
      3 m
      5 m
    • Empty weight
      7559 kg
      11339 kg
    • Max. takeoff weight (Gross weight)
      11249 kg
      16874 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
      20 per.
      32 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      167 km/h
      251 km/h
    • Сruise Speed
      186 km/h
      280 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
      3360 hp
      5040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2120 m
      3180 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      186 km
      280 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
      220 m/min
      332 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
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      123 qt
      185 qt
    • Price
      41 USD
      750000000 USD

Sikorsky CH-37 Mojave

TypeHelicopter
Company

Sikorsky Aircraft Corporation

Geometry
Length (m)
1.9
 
19.6
88.7
Height (m)
0.6
 
6.7
50.1
Rotors
Main rotor diameter (m)
1.2
 
22.0
62
Tail rotor diameter (m)
0.8
 
4.6
4.9
Weights
Empty weight (kg)
8
 
9,448.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
14,061.4
575,000
Capacity
Crew (per.)
1
 
3
112
Capacity passengers (per.)
1
 
26
400
or 24 stretchers
Speeds
Max. Speed (km/h)
25
 
209
28,165
Сruise Speed (km/h)
52
 
233
3,087
with maximum payload
Power
Total Power (hp)
0.4
 
4,200
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
2,650
161,544
Range (Ferry range) (km)
4
 
233
40,700
with maximum payload
Dynamic Performance
Rate of climb (m/min)
1.9
 
276
36,000
Stat
Number built (qt)
0
 
154
43,000
Introduction 1953
First flight 1953
Stop production 1960

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