Search filter

    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      8 m
      13 m
    • Wing loading
      171 kg/m2
      257 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
      6329 kg
      9495 kg
    • Max. takeoff weight (Gross weight)
      10186 kg
      15280 kg
    • Loaded weight
      8870 kg
      13306 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
      1272 km/h
      1908 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
      56 kN/kg
      86 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      36 kN
      54 kN
    • Service ceiling
      14020 m
      21032 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1718 km
      2578 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
      5054 m/min
      7583 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      3 qt
      5 qt
    • Rockets
      57 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      3 qt
      5 qt
    • Price
      41 USD
      750000000 USD

Douglas F5D Skylancer

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
16.4
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
10.2
95
Wing loading (kg/m2)
3.1
 
214
829
Weights
Empty weight (kg)
8
 
7,912.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,733.3
575,000
Loaded weight (kg)
5
 
11,088
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,590
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.7
2.1
Afterburning thrust (kN/kg)
29.4
 
71
980
1 powerplant
Thrust (kN)
1.5
 
45
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
17,526
161,544
Range (Ferry range) (km)
4
 
2,148
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
6,318.5
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) cannon
Missiles (qt)
1
 
2
24
AIM-7B Sparrow
1
 
4
24
AIM-9 Sidewinder or
Rockets (qt)
1
 
72
76
2 in (51 mm) rockets
Stat
Number built (qt)
0
 
4
43,000
Introduction 1956
First flight 21.04.1956

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