Search filter

    • Year
      1906
      2018
    • Length
      17 m
      26 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      51 m2
      77 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      204 kg/m2
      306 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
      8861 kg
      13293 kg
    • Max. takeoff weight (Gross weight)
      13880 kg
      20820 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 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
      1964 km/h
      2946 km/h
    • Сruise Speed
      52 km/h
      3087 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      87 kN
      131 kN
    • Service ceiling
      13600 m
      20400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2320 km
      3480 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
      7071 m/min
      10608 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 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
      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
      273 qt
      411 qt
    • Price
      3760000 USD
      5640000 USD

Convair Convair F-106 Delta Dart

TypeAircraft
Company

Consolidated Vultee Convair

General Dynamics

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
21.6
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wing area (m2)
1.1
 
64
925
Wingspan (Beam) (m)
0.1
 
11.7
95
Wing loading (kg/m2)
3.1
 
255
829
Weights
Empty weight (kg)
8
 
11,076.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
17,350
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
2,455
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.7
2.1
Thrust (kN)
1.5
 
109
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
17,000
161,544
Range (Ferry range) (km)
4
 
2,900
40,700
combat
Dynamic Performance
Rate of climb (m/min)
1.9
 
8,839.2
36,000
Time to altitude (min)
0.6
 
6.9
105
16065
Combat
Guns (qt)
1
 
1
18
20 mm caliber M61A1 Vulcan 6-barreled rotary cannon (After 1972 refit)
Stat
Number built (qt)
0
 
342
43,000
Price (USD)
41.5
 
4.7 million
750.0 million
Introduction 1956
First flight 26.12.1956
Stop production 01.08.1988

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