Search filter

    • Year
      1906
      2018
    • Length
      22 m
      34 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      170 m2
      256 m2
    • Wingspan (Beam)
      38 m
      58 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
      11355 kg
      17033 kg
    • Max. takeoff weight (Gross weight)
      22498 kg
      33748 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      6 per.
      10 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      42 per.
      64 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      224 km/h
      338 km/h
    • Max. Speed
      234 km/h
      352 km/h
    • Сruise Speed
      200 km/h
      300 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
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4704 m
      7056 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3864 km
      5796 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

Martin 156

TypeAircraft
Company

Glenn L. Martin Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
28.1
88.7
Height (m)
0.6
 
8.3
50.1
Wings
Wing area (m2)
1.1
 
212.8
925
Wingspan (Beam) (m)
0.1
 
47.9
95
Weights
Empty weight (kg)
8
 
14,193.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
28,123
575,000
Capacity
Crew (per.)
1
 
8
112
Capacity passengers (per.)
1
 
53
400
Speeds
Ground Speed (km/h)
96.6
 
281
1,500
Max. Speed (km/h)
25
 
293
28,165
Сruise Speed (km/h)
52
 
250
3,087
Power
Total Power (hp)
0.4
 
4,000
60,000
4 powerplants 1000 hp each
Performance
Service ceiling (m)
0.6
 
5,880
161,544
Range (Ferry range) (km)
4
 
4,830
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1937
Stop production 1944

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