Search filter

    • Year
      1906
      2018
    • Length
      28 m
      42 m
    • Height
      0 m
      51 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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
      11596 kg
      17395 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      23586 kg
      35381 kg
    • Crew
      8 per.
      12 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
      305 km/h
      458 km/h
    • Сruise Speed
      180 km/h
      271 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
      12834 l
      19252 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 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
      1 kN
      1914 kN
    • Service ceiling
      0 m
      161544 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      4119 km
      6180 km
    • Endurance
      19 h
      29 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
      180 m/min
      271 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
      4416 kg
      6624 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Martin XB-16

Company

Glenn L. Martin Company

Scheme

Concept

Twin-boom

Geometry
Length (m)
1.9
 
35
88.7
Weights
Empty weight (kg)
8
 
14,495.5
276,800
Loaded weight (kg)
5
 
29,483.5
242,500
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
381.4
28,165
at 6100 m
Сruise Speed (km/h)
52
 
225.3
3,087
Fuel
Fuel Capacity (l)
23
 
16,042.5
320,000
Power
Power/mass (hp/kg)
0.0
 
0.1
22.1
Performance
Сombat radius (km)
277
 
5,149.9
7,210
Endurance (h)
0.0
 
24
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
225.6
36,000
Combat
Bombs weight (kg)
2
 
5,520
39,000
Stat

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