Search filter

    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      5 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      48 m2
      74 m2
    • Wingspan (Beam)
      17 m
      26 m
    • Wing loading
      182 kg/m2
      274 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
      8708 kg
      13064 kg
    • Max. takeoff weight (Gross weight)
      13426 kg
      20140 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      5 per.
      9 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
      347 km/h
      521 km/h
    • Max. Speed
      368 km/h
      552 km/h
    • Сruise Speed
      286 km/h
      430 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      133 km/h
      201 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
      3520 hp
      5280 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5120 m
      7681 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2574 km
      3862 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1480 km
      2220 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
      292 m/min
      440 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
      9 qt
      15 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
      4230 qt
      6346 qt
    • Price
      82127 USD
      123192 USD

Martin B-26 Marauder

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17.8
88.7
Height (m)
0.6
 
6.6
50.1
Wings
Wing area (m2)
1.1
 
61.2
925
Wingspan (Beam) (m)
0.1
 
21.7
95
Wing loading (kg/m2)
3.1
 
228
829
Weights
Empty weight (kg)
8
 
10,886.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
16,783
575,000
Capacity
Crew (per.)
1
 
7
112
2 pilots, bombardier, navigator/radio operator, 3 gunners
Speeds
Ground Speed (km/h)
96.6
 
434
1,500
Max. Speed (km/h)
25
 
460
28,165
at 1500 m
Сruise Speed (km/h)
52
 
358
3,087
Landing Speed (km/h)
68
 
167
270
Power
Total Power (hp)
0.4
 
4,400
60,000
2 powerplants 2200 hp
Performance
Service ceiling (m)
0.6
 
6,400.8
161,544
Range (Ferry range) (km)
4
 
3,218
40,700
Сombat radius (km)
277
 
1,850
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
366
36,000
Combat
Guns (qt)
1
 
12
18
.50 in (12.7 mm) Browning machine guns
Stat
Number built (qt)
0
 
5,288
43,000
Price (USD)
41.5
 
102,659.3
750.0 million
Introduction 1940
First flight 25.11.1940

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