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    • Year
      1906
      2018
    • Length
      17 m
      26 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      16 m
      26 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
      16 m
      26 m
    • Rotor number
      1 qt
      3 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
      8800 kg
      13200 kg
    • Max. takeoff weight (Gross weight)
      12664 kg
      18996 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      2800 kg
      4200 kg
    • Capacity passengers
      32 per.
      48 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      140 km/h
      210 km/h
    • Сruise Speed
      120 km/h
      180 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
      2720 hp
      4080 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2160 m
      3240 m
    • Static ceiling
      2160 m
      3240 m
    • Range (Ferry range)
      212 km
      318 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
      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
      32 qt
      48 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-24

TypeHelicopter
Company

SC A.S. Yakovlev Design Bureau

Geometry
Length (m)
1.9
 
21.3
88.7
Height (m)
0.6
 
6.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
21
95
Rotors
Main rotor diameter (m)
1.2
 
21
62
Rotor number (qt)
1
 
2
8
Weights
Empty weight (kg)
8
 
11,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,830
575,000
Capacity
Crew (per.)
1
 
4
112
two pilots, flight engineer and radio operator
Payload (kg)
23
 
3,500
122,470
Capacity passengers (per.)
1
 
40
400
or 18 stretchers
Speeds
Max. Speed (km/h)
25
 
175
28,165
Сruise Speed (km/h)
52
 
150
3,087
Power
Total Power (hp)
0.4
 
3,400
60,000
2 powerplants 1700 hp each
Performance
Service ceiling (m)
0.6
 
2,700
161,544
Static ceiling (m)
3
 
2,700
5,485
Range (Ferry range) (km)
4
 
265
40,700
Stat
Number built (qt)
0
 
40
43,000
Introduction 1952
First flight 03.07.1952

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