Search filter

    • Year
      1906
      2018
    • Length
      26 m
      41 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      12 m
      20 m
    • Wing loading
      331 kg/m2
      497 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
      19568 kg
      29352 kg
    • Max. takeoff weight (Gross weight)
      37274 kg
      55912 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
      2051 km/h
      3077 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
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      195 kN
      293 kN
    • Service ceiling
      10924 m
      16387 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3928 km
      5892 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
      121 m/min
      183 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
      2 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

Martin 316

TypeAircraft
Company

Glenn L. Martin Company

Geometry
Length (m)
1.9
 
33.4
88.7
Height (m)
0.6
 
7.8
50.1
Wings
Wingspan (Beam) (m)
0.1
 
16.2
95
Wing loading (kg/m2)
3.1
 
414
829
Weights
Empty weight (kg)
8
 
24,460
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
46,593.0
575,000
Speeds
Max. Speed (km/h)
25
 
2,564
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.7
2.1
Thrust (kN)
1.5
 
244
1,914
2 powerplants 122 kN each
Performance
Service ceiling (m)
0.6
 
13,655.0
161,544
Range (Ferry range) (km)
4
 
4,910
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
152.4
36,000
Combat
Guns (qt)
1
 
1
18
20 mm (0.79 in) M61 Vulcan rotary cannon with 1,100 rounds in tail
Stat

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