Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      11 m2
      18 m2
    • Wingspan (Beam)
      4 m
      8 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
      3547 kg
      5321 kg
    • Max. takeoff weight (Gross weight)
      4956 kg
      7436 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      435 kg
      654 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      584 km/h
      876 km/h
    • Сruise Speed
      520 km/h
      780 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3520 hp
      5280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      418 km
      628 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
      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
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Curtiss-Wright C-143

TypeAircraft
Company

Curtiss-Wright

Scheme

High wing

Low wing

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
5.2
50.1
Wings
Wing area (m2)
1.1
 
14.4
925
Wingspan (Beam) (m)
0.1
 
5.9
95
forward
Weights
Empty weight (kg)
8
 
4,433.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,196.1
575,000
Capacity
Crew (per.)
1
 
2
112
Payload (kg)
23
 
544.3
122,470
Speeds
Max. Speed (km/h)
25
 
730
28,165
Сruise Speed (km/h)
52
 
650
3,087
Power
Total Power (hp)
0.4
 
4,400
60,000
2 powerplants 2200 hp each
Performance
Range (Ferry range) (km)
4
 
523
40,700
Stat
Number built (qt)
0
 
2
43,000
Introduction 1964
First flight 01.11.1963

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