Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      5 m
      8 m
    • Wing loading
      128 kg/m2
      194 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
      3772 kg
      5659 kg
    • Max. takeoff weight (Gross weight)
      4132 kg
      6199 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 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
      22532 km/h
      28165 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      258 kN
      388 kN
    • Service ceiling
      129235 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      32560 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
      24384 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
      43000 qt
    • Price
      41 USD
      750000000 USD

Boeing X-20 Dyna-Soar

TypeAircraft
Company

Boeing

Scheme

Concept

Low wing

Monoplane

Geometry
Length (m)
1.9
 
10.8
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
32.1
925
Wingspan (Beam) (m)
0.1
 
6.3
95
Wing loading (kg/m2)
3.1
 
161
829
Weights
Empty weight (kg)
8
 
4,715.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,165.1
575,000
Speeds
Max. Speed (km/h)
25
 
28,165
28,165
Power
Thrust (kN)
1.5
 
323
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
161,544
161,544
Range (Ferry range) (km)
4
 
40,700
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
30,480
36,000
Stat
Introduction 1963

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