Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      11 m2
      18 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      123 kg/m2
      185 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
      1244 kg
      1866 kg
    • Max. takeoff weight (Gross weight)
      2040 kg
      3060 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      792 kg
      1190 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
      528 km/h
      792 km/h
    • Сruise Speed
      438 km/h
      658 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
      804 l
      1208 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
      7 kN
      11 kN
    • Service ceiling
      12902 m
      19354 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      772 km
      1158 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      340 m
      510 m
    • Landing roll
      360 m
      540 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      864 m/min
      1296 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
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-30 (1960)

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.1
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
14.3
925
Wingspan (Beam) (m)
0.1
 
9.4
95
Wing loading (kg/m2)
3.1
 
154
829
Weights
Empty weight (kg)
8
 
1,555
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,550
575,000
Capacity
Crew (per.)
1
 
2
112
student and instructor
Useful load (kg)
26.4
 
991
90,700
Speeds
Max. Speed (km/h)
25
 
660
28,165
Сruise Speed (km/h)
52
 
548
3,087
Fuel
Fuel Capacity (l)
23
 
1,006
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
8.8
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
16,127.9
161,544
Range (Ferry range) (km)
4
 
965
40,700
Takeoff roll (m)
20
 
425
3,200
Landing roll (m)
20
 
450
2,570
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,080
36,000
Stat
Number built (qt)
0
 
4
43,000
Introduction 1960
First flight 20.05.1960

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