Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      8 m
      12 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
      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
      4240 kg
      6360 kg
    • Max. takeoff weight (Gross weight)
      7120 kg
      10680 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
      3 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      720 km/h
      1080 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
      2600 l
      3900 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
      0 hp
      60000 hp
    • Thrust
      83 kN
      125 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      1520 m
      2280 m
    • Range (Ferry range)
      296 km
      444 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
      6720 m/min
      10080 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
      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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-36

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
17
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
17
925
Wingspan (Beam) (m)
0.1
 
10
95
Weights
Empty weight (kg)
8
 
5,300
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,900
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
2
2,576
1
 
2
2,576
with a capacity of 100kg
Speeds
Max. Speed (km/h)
25
 
900
28,165
Fuel
Fuel Capacity (l)
23
 
3,606.1
320,000
23
 
3,250
320,000
Power
Thrust (kN)
1.5
 
104
1,914
2 powerplants 52 kN each
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Static ceiling (m)
3
 
1,900
5,485
Range (Ferry range) (km)
4
 
370
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
8,400
36,000
Combat
Guns (qt)
1
 
1
18
23 mm (0.91 in) GSh-23L cannon
Stat
Number built (qt)
0
 
4
43,000
Introduction 1963
First flight 09.01.1963

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