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    • Year
      1906
      2018
    • Length
      25 m
      39 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      27 m
      42 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
      17424 kg
      26137 kg
    • Max. takeoff weight (Gross weight)
      34690 kg
      52037 kg
    • Loaded weight
      33091 kg
      49637 kg
    • Crew
      2 per.
      4 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
      701 km/h
      1053 km/h
    • Сruise Speed
      565 km/h
      849 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
      0 hp
      60000 hp
    • Thrust
      56 kN
      86 kN
    • Service ceiling
      9753 m
      14631 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3696 km
      5546 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      8000 kg
      12000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      3920000 USD
      5880000 USD

Convair 109

TypeAircraft
Company

Consolidated Vultee Convair

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
32.3
88.7
Height (m)
0.6
 
8.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
34.5
95
Weights
Empty weight (kg)
8
 
21,780.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
43,363.4
575,000
Loaded weight (kg)
5
 
41,364
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
877
28,165
at 4580 m
Сruise Speed (km/h)
52
 
707
3,087
at 10700 m
Power
Thrust (kN)
1.5
 
71.2
1,914
4 powerplants 17,8 kN each
Performance
Service ceiling (m)
0.6
 
12,192
161,544
Range (Ferry range) (km)
4
 
4,621
40,700
Combat
Guns (qt)
1
 
2
18
.50 in (12.7 mm) M2 Browning machine guns
Bombs weight (kg)
2
 
10,000
39,000
Stat
Number built (qt)
0
 
1
43,000
Price (USD)
41.5
 
4.9 million
750.0 million
Introduction 1947
First flight 02.04.1947
Stop production 1947

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