Search filter

    • Year
      1906
      2018
    • Length
      31 m
      48 m
    • Height
      8 m
      14 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      148 m2
      223 m2
    • Wingspan (Beam)
      29 m
      44 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      9
    • 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
      34110 kg
      51166 kg
    • Max. takeoff weight (Gross weight)
      70034 kg
      105052 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      8708 kg
      13064 kg
    • Capacity passengers
      88 per.
      132 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      792 km/h
      1188 km/h
    • Stall Speed
      143 km/h
      215 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
      37968 l
      56952 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
      0 hp
      60000 hp
    • Thrust
      166 kN
      250 kN
    • Service ceiling
      9997 m
      14997 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3544 km
      5316 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
      52 qt
      78 qt
    • Price
      41 USD
      750000000 USD

Convair 880

TypeAircraft
Company

Consolidated Vultee Convair

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
39.4
88.7
Height (m)
0.6
 
11
50.1
Wings
Wing area (m2)
1.1
 
185.8
925
Wingspan (Beam) (m)
0.1
 
36.6
95
Aspect ratio
1.7
 
7.2
25.6
Weights
Empty weight (kg)
8
 
42,637.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
87,543.3
575,000
Capacity
Crew (per.)
1
 
3
112
Payload (kg)
23
 
10,886.2
122,470
Capacity passengers (per.)
1
 
110
400
Speeds
Сruise Speed (km/h)
52
 
990
3,087
at 6860 m
Stall Speed (km/h)
40
 
179
257.7
Fuel
Fuel Capacity (l)
23
 
47,460
320,000
Power
Thrust (kN)
1.5
 
207.8
1,914
4 powerplants 51,95 kN each
Performance
Service ceiling (m)
0.6
 
12,496.8
161,544
max cruise altitude
Range (Ferry range) (km)
4
 
4,430
40,700
Stat
Number built (qt)
0
 
65
43,000
Introduction 1959
First flight 27.01.1959

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