Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      8 m
      12 m
    • Wing loading
      134 kg/m2
      202 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
      1915 kg
      2873 kg
    • Max. takeoff weight (Gross weight)
      2306 kg
      3460 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
      1 qt
      2576 qt
    • Ground Speed
      424 km/h
      638 km/h
    • Max. Speed
      473 km/h
      711 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
      29 kN/kg
      980 kN/kg
    • Total Power
      943 hp
      1416 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8040 m
      12060 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      560 km
      840 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
      739 m/min
      1109 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
      3 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
      6960 qt
      10440 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-1

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.5
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
17.2
925
Wingspan (Beam) (m)
0.1
 
10
95
Wing loading (kg/m2)
3.1
 
168
829
Weights
Empty weight (kg)
8
 
2,394
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,883
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
531
1,500
Max. Speed (km/h)
25
 
592
28,165
Power
Total Power (hp)
0.4
 
1,179.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,050
161,544
Range (Ferry range) (km)
4
 
700
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
924
36,000
Combat
Guns (qt)
1
 
2
18
1 × 20 mm (0.8 in) ShVAK cannon, 1 × 12.7 mm (0.5 in) Berezin UBS machine gun
Stat
Number built (qt)
0
 
8,700
43,000
Introduction 1942
First flight 13.01.1940
Stop production 1950

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