Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 m2
    • Wingspan (Beam)
      9 m
      15 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
      492 kg
      740 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      768 kg
      1154 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      3 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      134 km/h
      203 km/h
    • Сruise Speed
      104 km/h
      156 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
      29 kN/kg
      980 kN/kg
    • Total Power
      80 hp
      120 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3680 m
      5520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      572 km
      858 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
      5 min
      8 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
      102 qt
      154 qt
    • Price
      41 USD
      750000000 USD

Yakovlev AIR-6

Company

SC A.S. Yakovlev Design Bureau

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
7.8
88.7
Wings
Wing area (m2)
1.1
 
19.8
925
Wingspan (Beam) (m)
0.1
 
12.1
95
Weights
Empty weight (kg)
8
 
616
276,800
Loaded weight (kg)
5
 
961
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
2
400
Speeds
Max. Speed (km/h)
25
 
168.5
28,165
Сruise Speed (km/h)
52
 
130
3,087
Power
Total Power (hp)
0.4
 
100
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,600
161,544
Range (Ferry range) (km)
4
 
715
40,700
Dynamic Performance
Time to altitude (min)
0.6
 
6.6
105
to 1000 m
Stat
Number built (qt)
0
 
128
43,000
First flight 1932

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