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    • Year
      1906
      2018
    • Length
      23 m
      36 m
    • Height
      7 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      114 m2
      172 m2
    • Wingspan (Beam)
      44 m
      68 m
    • Wing loading
      172 kg/m2
      258 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      3
    • 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
      20161 kg
      30242 kg
    • Max. takeoff weight (Gross weight)
      64188 kg
      96284 kg
    • Loaded weight
      5 kg
      242500 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
      784 km/h
      1176 km/h
    • Max. Speed
      9600 km/h
      14400 km/h
    • Сruise Speed
      788 km/h
      1182 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
      1 kN/kg
    • Afterburning thrust
      221 kN/kg
      333 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      169 kN
      254 kN
    • Service ceiling
      15459 m
      23190 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      2576 km
      3864 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
      4224 m/min
      6336 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
      2 qt
    • Bombs
      3 qt
      5 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
      92 qt
      140 qt
    • Price
      9952000 USD
      14928000 USD

Convair Model 4

TypeAircraft
Company

Consolidated Vultee Convair

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
29.5
88.7
Height (m)
0.6
 
8.9
50.1
Wings
Wing area (m2)
1.1
 
143.3
925
Wingspan (Beam) (m)
0.1
 
56
95
Wing loading (kg/m2)
3.1
 
215
829
Aspect ratio
1.7
 
2.1
25.6
Weights
Empty weight (kg)
8
 
25,201.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
80,236.0
575,000
Capacity
Crew (per.)
1
 
3
112
pilot; observer (navigator, radar operator, bombardier); defense system operator (DSO; electronic countermeasures operator and pilot assistant)
Speeds
Ground Speed (km/h)
96.6
 
980
1,500
Max. Speed (km/h)
25
 
12,000
28,165
Сruise Speed (km/h)
52
 
985
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.0
2.1
Afterburning thrust (kN/kg)
29.4
 
277.2
980
4 powerplants 69,3 kN each
Thrust (kN)
1.5
 
211.6
1,914
4 powerplants 52,9 kN each
Performance
Service ceiling (m)
0.6
 
19,324.3
161,544
Сombat radius (km)
277
 
3,220
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
5,280
36,000
at gross weight
Combat
Guns (qt)
1
 
1
18
20 mm (0.79 in) T171 cannon
Bombs (qt)
1
 
4
250
B43 or B61 nuclear bombs
Stat
Number built (qt)
0
 
116
43,000
Price (USD)
41.5
 
12.4 million
750.0 million
Introduction 1956
First flight 11.11.1956
Stop production 31.01.1970

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