Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      35 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      308 kg/m2
      464 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
      5836 kg
      8754 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 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
      960 km/h
      1440 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      31 kN
      48 kN
    • Service ceiling
      12800 m
      19200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1760 km
      2640 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
      3 qt
      5 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
      8 qt
      12 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-26

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
17.2
88.7
Wings
Wing area (m2)
1.1
 
28.9
925
Wingspan (Beam) (m)
0.1
 
11.0
95
Wing loading (kg/m2)
3.1
 
386
829
Weights
Empty weight (kg)
8
 
7,295
276,800
Capacity
Crew (per.)
1
 
2
112
pilot and bombardier
Speeds
Max. Speed (km/h)
25
 
1,200
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
39.2
1,914
2 powerplats 19,6 kN each
Performance
Service ceiling (m)
0.6
 
16,000
161,544
Range (Ferry range) (km)
4
 
2,200
40,700
Combat
Guns (qt)
1
 
4
18
23 mm Nudelman NR-23 cannon with 1,200 rounds
Stat
Number built (qt)
0
 
10
43,000
Introduction 1956
First flight 1956

Similar aircraft

Get more

Comments