Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      18 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      48 kg/m2
      73 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
      1 m
      62 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
      600 kg
      900 kg
    • Max. takeoff weight (Gross weight)
      728 kg
      1092 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 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
      320 km/h
      480 km/h
    • Сruise Speed
      216 km/h
      324 km/h
    • Stall Speed
      80 km/h
      120 km/h
    • Landing Speed
      88 km/h
      132 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      360 km/h
      540 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
      320 hp
      480 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      400 km
      600 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      1 h
    • Takeoff roll
      80 m
      120 m
    • Landing roll
      200 m
      300 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      7 G
      9 G
    • Rate of climb
      542 m/min
      814 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
      251 qt
      377 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-50 (1975)

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.8
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
15
925
Wingspan (Beam) (m)
0.1
 
9.5
95
Wing loading (kg/m2)
3.1
 
60.7
829
Weights
Empty weight (kg)
8
 
750
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
910
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
400
28,165
Сruise Speed (km/h)
52
 
270
3,087
Stall Speed (km/h)
40
 
100
257.7
Landing Speed (km/h)
68
 
110
270
Never exceed speed (km/h)
108.0
 
450
1,050
Power
Total Power (hp)
0.4
 
400
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
500
40,700
Endurance (h)
0.0
 
0.8
150
Takeoff roll (m)
20
 
100
3,200
Landing roll (m)
20
 
250
2,570
Dynamic Performance
Load factor from (G)
2
 
9
9
Rate of climb (m/min)
1.9
 
678
36,000
Stat
Number built (qt)
0
 
314
43,000
Introduction 1972
First flight 25.06.1975

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