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    • Year
      1906
      2018
    • Length
      60 m
      89 m
    • Height
      8 m
      13 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      90 m2
      137 m2
    • Wingspan (Beam)
      26 m
      41 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
      12833 kg
      19251 kg
    • Max. takeoff weight (Gross weight)
      21772 kg
      32659 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      8708 kg
      13064 kg
    • Capacity passengers
      48 per.
      72 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      293 km/h
      441 km/h
    • Сruise Speed
      222 km/h
      334 km/h
    • Stall Speed
      121 km/h
      183 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      4000 hp
      6000 hp
    • Thrust
      20 kN
      32 kN
    • Service ceiling
      5145 m
      7718 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1332 km
      2000 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
      297 m/min
      447 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
      245 qt
      369 qt
    • Price
      41 USD
      750000000 USD

Fairchild C-123 Provider

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
76
88.7
Height (m)
0.6
 
10.4
50.1
Wings
Wing area (m2)
1.1
 
113.6
925
Wingspan (Beam) (m)
0.1
 
33.5
95
Weights
Empty weight (kg)
8
 
16,041.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
27,215.5
575,000
Capacity
Crew (per.)
1
 
4
112
Payload (kg)
23
 
10,886.2
122,470
Capacity passengers (per.)
1
 
60
400
Speeds
Max. Speed (km/h)
25
 
367
28,165
at 3050 m
Сruise Speed (km/h)
52
 
278
3,087
Stall Speed (km/h)
40
 
152
257.7
Power
Total Power (hp)
0.4
 
5,000
60,000
2 powerplants 2500 hp each
Thrust (kN)
1.5
 
26
1,914
2 powerplants 13 kN each
Performance
Service ceiling (m)
0.6
 
6,431.3
161,544
One engine failed
Range (Ferry range) (km)
4
 
1,666
40,700
with max payload
Dynamic Performance
Rate of climb (m/min)
1.9
 
371.9
36,000
Stat
Number built (qt)
0
 
307
43,000
Introduction 1949
First flight 14.10.1949
Stop production 1980

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