Search filter

    • Year
      1906
      2018
    • Length
      14 m
      23 m
    • Height
      4 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      8 m
      13 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
      9320 kg
      13980 kg
    • Max. takeoff weight (Gross weight)
      15600 kg
      23400 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      4 qt
      6 qt
    • Ground Speed
      1000 km/h
      1500 km/h
    • Max. Speed
      1440 km/h
      2160 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
      121 kN/kg
      183 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      86 kN
      130 kN
    • Service ceiling
      12400 m
      18600 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1680 km
      2520 km
    • Range PTB (Ferry range)
      2400 km
      3600 km
    • Сombat radius
      552 km
      828 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
      5 G
      9 G
    • Rate of climb
      12000 m/min
      18000 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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-141

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
18.4
88.7
Height (m)
0.6
 
5
50.1
Wings
Wing area (m2)
1.1
 
31.7
925
Wingspan (Beam) (m)
0.1
 
10.1
95
Weights
Empty weight (kg)
8
 
11,650
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
19,500
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
5
2,576
4 underwing and 1 fuselage hardpoints with a capacity of 2600 kg
Speeds
Ground Speed (km/h)
96.6
 
1,250
1,500
Max. Speed (km/h)
25
 
1,800
28,165
Power
Afterburning thrust (kN/kg)
29.4
 
152
980
Thrust (kN)
1.5
 
108
1,914
Performance
Service ceiling (m)
0.6
 
15,500
161,544
Range (Ferry range) (km)
4
 
2,100
40,700
Range PTB (Ferry range) (km)
720
 
3,000
10,000
Сombat radius (km)
277
 
690
7,210
Dynamic Performance
Load factor from (G)
2
 
7
9
Rate of climb (m/min)
1.9
 
15,000
36,000
Combat
Guns (qt)
1
 
1
18
30 mm GSh-301 cannon with 120 rounds
Stat
Number built (qt)
0
 
2
43,000
Introduction 1989
First flight 09.03.1987

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