Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      11 m2
      18 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      157 kg/m2
      237 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
      1481 kg
      2223 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2110 kg
      3166 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
      560 km/h
      840 km/h
    • Max. Speed
      628 km/h
      944 km/h
    • Сruise Speed
      551 km/h
      827 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
      472 l
      708 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
      7 kN
      11 kN
    • Service ceiling
      9600 m
      14400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      408 km
      612 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      408 km
      612 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
      1036 m/min
      1556 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
      3 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
      224 qt
      336 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-15

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
8.7
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
14.9
925
Wingspan (Beam) (m)
0.1
 
9.2
95
Wing loading (kg/m2)
3.1
 
197
829
Weights
Empty weight (kg)
8
 
1,852
276,800
Loaded weight (kg)
5
 
2,638
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
700
1,500
Max. Speed (km/h)
25
 
786
28,165
Сruise Speed (km/h)
52
 
689
3,087
Fuel
Fuel Capacity (l)
23
 
590
320,000
Power
Thrust (kN)
1.5
 
8.8
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,000
161,544
Range (Ferry range) (km)
4
 
510
40,700
Сombat radius (km)
277
 
510
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,296
36,000
Combat
Guns (qt)
1
 
2
18
23 mm Nudelman-Suranov NS-23 cannon with 60 rounds each
Stat
Number built (qt)
0
 
280
43,000
Introduction 1947
First flight 24.04.1946

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