Search filter

    • Year
      1906
      2018
    • Length
      14 m
      23 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      35 m2
    • Wingspan (Beam)
      9 m
      15 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
      6048 kg
      9072 kg
    • Max. takeoff weight (Gross weight)
      10880 kg
      16320 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      1028 km/h
      1542 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
      0 hp
      60000 hp
    • Thrust
      59 kN
      90 kN
    • Service ceiling
      13240 m
      19860 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1904 km
      2856 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      3 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
      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
      132 qt
      198 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-27

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
18.6
88.7
Wings
Wing area (m2)
1.1
 
28.9
925
Wingspan (Beam) (m)
0.1
 
11.8
95
Weights
Empty weight (kg)
8
 
7,560
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,600
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
1,285
28,165
Power
Thrust (kN)
1.5
 
74.4
1,914
2 powerplants 37,2
Performance
Service ceiling (m)
0.6
 
16,550
161,544
Range (Ferry range) (km)
4
 
2,380
40,700
Endurance (h)
0.0
 
2.5
150
Combat
Guns (qt)
1
 
1
18
23 mm Nudelman-Rikhter NR-23 cannon
Stat
Number built (qt)
0
 
165
43,000
+ prototypes
Introduction 1960
Stop production 1970

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