Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      17 m2
    • Wingspan (Beam)
      6 m
      11 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
      1584 kg
      2376 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2707 kg
      4061 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
      740 km/h
      1110 km/h
    • Max. Speed
      25 km/h
      28165 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      12 kN
      19 kN
    • Service ceiling
      11840 m
      17760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      960 km
      1440 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      3 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
      2256 m/min
      3384 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
      248 qt
      372 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-23

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
3.3
50.1
Wings
Wing area (m2)
1.1
 
13.7
925
Wingspan (Beam) (m)
0.1
 
8.7
95
Weights
Empty weight (kg)
8
 
1,980
276,800
Loaded weight (kg)
5
 
3,384
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
925
1,500
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Thrust (kN)
1.5
 
15.6
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
14,800
161,544
Range (Ferry range) (km)
4
 
1,200
40,700
Endurance (h)
0.0
 
2.3
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,820
36,000
Combat
Guns (qt)
1
 
2
18
23 mm Nudelman-Rikhter NR-23 with 90 rpg
Stat
Number built (qt)
0
 
310
43,000
Introduction 1947
First flight 08.07.1947
Stop production 1951

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