Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      6 m
      10 m
    • Wing loading
      340 kg/m2
      512 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
      3418 kg
      5128 kg
    • Max. takeoff weight (Gross weight)
      5539 kg
      8310 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
      1608 km/h
      2412 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      206 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
      760 l
      1140 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
      32 kN
      48 kN
    • Service ceiling
      4023 m
      6036 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      2704 m/min
      4056 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
      18 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
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

Douglas D558-II Skyrocket

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
12.8
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
16.3
925
Wingspan (Beam) (m)
0.1
 
7.6
95
Wing loading (kg/m2)
3.1
 
426
829
Weights
Empty weight (kg)
8
 
4,273.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,924.5
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,160
28,165
25
 
2,010
28,165
when air-launched
Stall Speed (km/h)
40
 
257.7
257.7
Fuel
Fuel Capacity (l)
23
 
950
320,000
of aviation fuel
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
jet
Thrust (kN)
1.5
 
40
1,914
2 powerplants 13 kN one and 27 kN another
Performance
Service ceiling (m)
0.6
 
5,029.2
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
6,827.5
36,000
1.9
 
3,380
36,000
under rocket power only
Stat
Number built (qt)
0
 
3
43,000
Introduction 1948
First flight 04.02.1948

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