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    • Year
      1906
      2018
    • Length
      17 m
      26 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      30 m2
      46 m2
    • Wingspan (Beam)
      10 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
      7976 kg
      11964 kg
    • Max. takeoff weight (Gross weight)
      16000 kg
      24000 kg
    • Loaded weight
      12000 kg
      18000 kg
    • Crew
      1 per.
      3 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
      96 km/h
      1500 km/h
    • Max. Speed
      1472 km/h
      2208 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
      3692 l
      5538 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
      99 kN/kg
      149 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      73 kN
      111 kN
    • Service ceiling
      13400 m
      20100 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2000 km
      3000 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
      1 m/min
      36000 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
      3 qt
      5 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
      944 qt
      1416 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-28

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
21.6
88.7
Height (m)
0.6
 
4.0
50.1
Wings
Wing area (m2)
1.1
 
37.6
925
Wingspan (Beam) (m)
0.1
 
12.5
95
Weights
Empty weight (kg)
8
 
9,970
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,000
575,000
Loaded weight (kg)
5
 
15,000
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
1,840
28,165
Fuel
Fuel Capacity (l)
23
 
4,615
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Afterburning thrust (kN/kg)
29.4
 
124
980
2 powerplants 62 kN each
Thrust (kN)
1.5
 
92
1,914
2 powerplants 46 kN each
Performance
Service ceiling (m)
0.6
 
16,750
161,544
Range (Ferry range) (km)
4
 
2,500
40,700
Endurance (h)
0.0
 
2.3
150
Combat
Missiles (qt)
1
 
4
24
2 × R-98M (AA-3 'Anab') air-to-air missiles, usually one R-98TM infrared and one R-98RM semi-active radar homing; 2 × K-13A (AA-2 'Atoll') short-range missiles (occasionally fitted)
Stat
Number built (qt)
0
 
1,180
43,000
Introduction 1962
First flight 05.03.1958
Stop production 1992

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