Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 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
      13 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
      760 kg
      1140 kg
    • Max. takeoff weight (Gross weight)
      1216 kg
      1824 kg
    • Loaded weight
      1040 kg
      1560 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
      96 km/h
      1500 km/h
    • Max. Speed
      184 km/h
      276 km/h
    • Сruise Speed
      154 km/h
      232 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
      180 l
      270 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
      204 hp
      308 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3200 m
      4800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      800 km
      1200 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
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Yakovlev Yak-112

TypeAircraft
Company

SC A.S. Yakovlev Design Bureau

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
7.0
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
17.0
925
Wingspan (Beam) (m)
0.1
 
10.3
95
Weights
Empty weight (kg)
8
 
950
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,520
575,000
Loaded weight (kg)
5
 
1,300
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
230
28,165
Сruise Speed (km/h)
52
 
193
3,087
Fuel
Fuel Capacity (l)
23
 
225
320,000
Power
Total Power (hp)
0.4
 
256
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,000
161,544
Range (Ferry range) (km)
4
 
1,000
40,700
Propellers
Propellers (qt)
1
 
1
8
Prop blade number (qt)
1
 
3
8
Stat
Introduction 1992
First flight 20.10.1992

Comments