Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      23 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      8
    • 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
      973 kg
      1461 kg
    • Max. takeoff weight (Gross weight)
      1320 kg
      1980 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
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      209 km/h
      315 km/h
    • Сruise Speed
      200 km/h
      300 km/h
    • Stall Speed
      91 km/h
      137 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      240 km/h
      360 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
      287 hp
      432 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      600 km
      900 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
      240 m/min
      360 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
      600 qt
      900 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-18T

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.4
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
18.8
925
Wingspan (Beam) (m)
0.1
 
11.2
95
Aspect ratio
1.7
 
6.6
25.6
Weights
Empty weight (kg)
8
 
1,217
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,650
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
262
28,165
Сruise Speed (km/h)
52
 
250
3,087
Stall Speed (km/h)
40
 
114
257.7
gear & flaps down
Never exceed speed (km/h)
108.0
 
300
1,050
Power
Total Power (hp)
0.4
 
359.3
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
without supplementary oxygen
Range (Ferry range) (km)
4
 
750
40,700
standard 180 liters fuel
Dynamic Performance
Rate of climb (m/min)
1.9
 
300
36,000
Stat
Number built (qt)
0
 
750
43,000
Introduction 1967
First flight 1967

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