Search filter

    • Year
      1906
      2018
    • Length
      16 m
      25 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      19 m2
    • Wingspan (Beam)
      5 m
      9 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
      5849 kg
      8775 kg
    • Max. takeoff weight (Gross weight)
      8650 kg
      12977 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
      900 km/h
      1350 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
      34 kN/kg
      52 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      24 kN
      36 kN
    • Service ceiling
      9265 m
      13899 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      640 km
      960 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
      1 m/min
      36000 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Douglas X-3 Stiletto

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
20.3
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
15.7
925
Wingspan (Beam) (m)
0.1
 
6.9
95
Weights
Empty weight (kg)
8
 
7,311.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,813.6
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,125
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Afterburning thrust (kN/kg)
29.4
 
43.2
980
2 powerplants 21,6 kN each
Thrust (kN)
1.5
 
30
1,914
2 powerplants 15 kN each
Performance
Service ceiling (m)
0.6
 
11,582.4
161,544
Range (Ferry range) (km)
4
 
800
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1952
First flight 15.10.1952
Stop production 23.05.1956

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