Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      35 m2
    • Wingspan (Beam)
      12 m
      19 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
      1008 kg
      1512 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2213 kg
      3321 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      219 km/h
      329 km/h
    • Сruise Speed
      113 km/h
      171 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
      384 l
      577 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
      520 hp
      780 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5560 m
      8340 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      389 km
    • Endurance
      3 h
      6 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
      365 m/min
      549 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Fairchild AU-23 Peacemaker

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
11.2
88.7
Height (m)
0.6
 
4.4
50.1
Wings
Wing area (m2)
1.1
 
28.8
925
Wingspan (Beam) (m)
0.1
 
15.1
95
Weights
Empty weight (kg)
8
 
1,260
276,800
Loaded weight (kg)
5
 
2,766.9
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
274
28,165
at take-off power at 1524 m
Сruise Speed (km/h)
52
 
142
3,087
Fuel
Fuel Capacity (l)
23
 
480.8
320,000
Power
Total Power (hp)
0.4
 
650
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,950
161,544
Сombat radius (km)
277
 
323.5
7,210
Endurance (h)
0.0
 
4.8
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
457
36,000
Stat
Introduction 1971

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