Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      101 m2
      152 m2
    • Wingspan (Beam)
      26 m
      40 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
      11760 kg
      17640 kg
    • Max. takeoff weight (Gross weight)
      16329 kg
      24494 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      348 km/h
      522 km/h
    • Сruise Speed
      222 km/h
      334 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
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5974 m
      8962 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4055 km
      6083 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1544 km
      2318 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
      286 m/min
      430 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
      2544 qt
      3818 qt
    • Price
      41 USD
      750000000 USD

Curtiss C-46 Commando

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
23.3
88.7
Height (m)
0.6
 
6.6
50.1
Wings
Wing area (m2)
1.1
 
126.3
925
Wingspan (Beam) (m)
0.1
 
32.9
95
Weights
Empty weight (kg)
8
 
14,700
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
20,411.7
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
435
28,165
at 4600 m
Сruise Speed (km/h)
52
 
278
3,087
Power
Total Power (hp)
0.4
 
4,000
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
7,467.6
161,544
Range (Ferry range) (km)
4
 
5,069
40,700
at 278 km/h
Сombat radius (km)
277
 
1,931
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
358.1
36,000
Stat
Number built (qt)
0
 
3,181
43,000
Introduction 1940
First flight 26.03.1940

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