Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      0 m
      51 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
      11 m
      18 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
      2 m
      4 m
    • Empty weight
      1444 kg
      2166 kg
    • Max. takeoff weight (Gross weight)
      1744 kg
      2616 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
      136 km/h
      204 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
      335 hp
      504 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4200 m
      6300 m
    • Static ceiling
      2176 m
      3264 m
    • Range (Ferry range)
      260 km
      390 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-100

TypeHelicopter
Company

SC A.S. Yakovlev Design Bureau

Geometry
Length (m)
1.9
 
13.9
88.7
Rotors
Main rotor diameter (m)
1.2
 
14.5
62
1.2
 
14.5
62
Tail rotor diameter (m)
0.8
 
2.6
4.9
Weights
Empty weight (kg)
8
 
1,805
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,180
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
170
28,165
Power
Total Power (hp)
0.4
 
419.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,250
161,544
Static ceiling (m)
3
 
2,720
5,485
Range (Ferry range) (km)
4
 
325
40,700
Stat
Number built (qt)
0
 
2
43,000
Introduction 1948
First flight 08.05.1948

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