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    • Year
      1906
      2018
    • Length
      29 m
      44 m
    • Height
      7 m
      12 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      120 m2
      180 m2
    • Wingspan (Beam)
      27 m
      42 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
      26400 kg
      39600 kg
    • Max. takeoff weight (Gross weight)
      46000 kg
      69000 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
      96 per.
      144 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      648 km/h
      972 km/h
    • Сruise Speed
      648 km/h
      972 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
      18500 l
      27750 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
      153 kN
      230 kN
    • Service ceiling
      7680 m
      11520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3200 km
      4800 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
      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
      148 qt
      222 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-42

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
36.4
88.7
Height (m)
0.6
 
9.8
50.1
Wings
Wing area (m2)
1.1
 
150
925
Wingspan (Beam) (m)
0.1
 
34.9
95
Weights
Empty weight (kg)
8
 
33,000
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
57,500
575,000
Capacity
Crew (per.)
1
 
3
112
two pilots plus optional flight engineer
Capacity passengers (per.)
1
 
120
400
But usually 8 first class and 96 economy class
Speeds
Max. Speed (km/h)
25
 
810
28,165
maximum cruise
Сruise Speed (km/h)
52
 
810
3,087
Fuel
Fuel Capacity (l)
23
 
23,125
320,000
Power
Thrust (kN)
1.5
 
191.3
1,914
3 powerplants 63,75 kN each
Performance
Service ceiling (m)
0.6
 
9,600
161,544
Range (Ferry range) (km)
4
 
4,000
40,700
with maximum fuel
Stat
Number built (qt)
0
 
185
43,000
as of 1 January 1995
Introduction 1980
First flight 07.03.1975

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