Search filter

    • Year
      1906
      2018
    • Length
      18 m
      28 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      92 m2
    • Wingspan (Beam)
      22 m
      34 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
      2 qt
      4 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
      9233 kg
      13850 kg
    • Max. takeoff weight (Gross weight)
      21097 kg
      31647 kg
    • Loaded weight
      14696 kg
      22045 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      32 per.
      48 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      405 km/h
      609 km/h
    • Сruise Speed
      360 km/h
      541 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
      3028 l
      4543 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
      3840 hp
      5760 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3901 m
      5853 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2920 km
      4380 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
      369 m/min
      555 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
      2 qt
      4 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
      944 qt
      1418 qt
    • Price
      41 USD
      750000000 USD

Convair CV-240

TypeAircraft
Company

Consolidated Vultee Convair

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
22.8
88.7
Height (m)
0.6
 
8.2
50.1
Wings
Wing area (m2)
1.1
 
75.9
925
Wingspan (Beam) (m)
0.1
 
28.0
95
Rotors
Rotor number (qt)
1
 
3
8
Weights
Empty weight (kg)
8
 
11,541.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
26,372
575,000
Loaded weight (kg)
5
 
18,370.5
242,500
Capacity
Crew (per.)
1
 
2
112
2 or 3 flight deck crew
Capacity passengers (per.)
1
 
40
400
Speeds
Max. Speed (km/h)
25
 
506.9
28,165
Сruise Speed (km/h)
52
 
450.6
3,087
Fuel
Fuel Capacity (l)
23
 
3,785.4
320,000
Power
Total Power (hp)
0.4
 
4,800
60,000
2 powerplants 2400 hp each
Performance
Service ceiling (m)
0.6
 
4,877
161,544
Range (Ferry range) (km)
4
 
3,650
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
462
36,000
Propellers
Prop blade number (qt)
1
 
3
8
Stat
Number built (qt)
0
 
1,181
43,000
Introduction 1955
First flight 16.03.1947

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