Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      37 m2
      57 m2
    • Wingspan (Beam)
      45 m
      69 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
      19964 kg
      29948 kg
    • Max. takeoff weight (Gross weight)
      18143 kg
      27216 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
      8 qt
      14 qt
    • Ground Speed
      564 km/h
      848 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      507 km/h
      761 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
      64 kN
      97 kN
    • Service ceiling
      10972 m
      16460 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3159 km
      4739 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      584 km
      878 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
      1463 m/min
      2195 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
      2 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
      572 qt
      860 qt
    • Price
      9440000 USD
      14160000 USD

Fairchild Fairchild-Republic A-10 Thunderbolt II

TypeAircraft
Company

Fairchild Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
16.3
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
47.0
925
Wingspan (Beam) (m)
0.1
 
57
95
Weights
Empty weight (kg)
8
 
24,956
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
22,679.6
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
11
2,576
8× under-wing and 3× under-fuselage pylon stations
Speeds
Ground Speed (km/h)
96.6
 
706
1,500
Сruise Speed (km/h)
52
 
634
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
80.6
1,914
2 powerplants 40,32 hp each
Performance
Service ceiling (m)
0.6
 
13,716
161,544
Range (Ferry range) (km)
4
 
3,949
40,700
Сombat radius (km)
277
 
731
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,828.8
36,000
Combat
Guns (qt)
1
 
1
18
30 mm (1.18 in) GAU-8/A Avenger Gatling cannon with 1,174 rounds
Stat
Number built (qt)
0
 
716
43,000
Price (USD)
41.5
 
11.8 million
750.0 million
Introduction 1972
First flight 10.05.1972

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