Search filter

    • Year
      1906
      2018
    • Length
      16 m
      25 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      56 m2
      84 m2
    • Wingspan (Beam)
      20 m
      30 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
      7520 kg
      11280 kg
    • Max. takeoff weight (Gross weight)
      12400 kg
      18600 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      25 per.
      39 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      440 km/h
      660 km/h
    • Сruise Speed
      393 km/h
      591 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
      3000 l
      4500 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
      35 kN
      53 kN
    • Service ceiling
      6400 m
      9600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1440 km
      2160 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
      384 m/min
      576 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
      808 qt
      1214 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-40

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
20.4
88.7
Height (m)
0.6
 
6.5
50.1
Wings
Wing area (m2)
1.1
 
70
925
Wingspan (Beam) (m)
0.1
 
25
95
Weights
Empty weight (kg)
8
 
9,400
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,500
575,000
Capacity
Crew (per.)
1
 
3
112
two pilots, one flight engineer
Capacity passengers (per.)
1
 
32
400
Speeds
Max. Speed (km/h)
25
 
550
28,165
at 7000 m max cruise
Сruise Speed (km/h)
52
 
492
3,087
Fuel
Fuel Capacity (l)
23
 
3,750
320,000
Power
Thrust (kN)
1.5
 
44.1
1,914
3 powerplants 14,7 kN
Performance
Service ceiling (m)
0.6
 
8,000
161,544
Range (Ferry range) (km)
4
 
1,800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
480
36,000
Stat
Number built (qt)
0
 
1,011
43,000
Introduction 01.09.1968
First flight 21.10.1966

Similar aircraft

Get more

Museums on map

Museums

Comments