Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      41 m2
      63 m2
    • Wingspan (Beam)
      8 m
      13 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
      5814 kg
      8723 kg
    • Max. takeoff weight (Gross weight)
      9839 kg
      14760 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
      929 km/h
      1395 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
      13600 m
      20400 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      880 km
      1320 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
      4462 m/min
      6694 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
      4 qt
      8 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      725 kg
      1089 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      337 qt
      507 qt
    • Price
      41 USD
      750000000 USD

Douglas F4D Skyray

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
13.8
88.7
Height (m)
0.6
 
4.0
50.1
Wings
Wing area (m2)
1.1
 
51.7
925
Wingspan (Beam) (m)
0.1
 
10.2
95
Weights
Empty weight (kg)
8
 
7,268.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,299.6
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,162
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
 
17,000
161,544
Range (Ferry range) (km)
4
 
1,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
5,577.8
36,000
Combat
Guns (qt)
1
 
4
18
20 mm Colt Mk 12 cannon
Missiles (qt)
1
 
4
24
AIM-9 Sidewinder air-to-air missiles
Rockets (qt)
1
 
4
76
pods of 19 2.75 in (70 mm) unguided rockets
1
 
6
76
pods of 7 2.75 in (70 mm) unguided rockets or
Bombs weight (kg)
2
 
907
39,000
bombs
Stat
Number built (qt)
0
 
422
43,000
Introduction 1951
First flight 23.01.1951
Stop production 1964

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