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    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      56 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      190 kg/m2
      286 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
      3 qt
      5 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
      5536 kg
      8305 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      9339 kg
      14009 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      12 qt
      18 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      430 km/h
      646 km/h
    • Сruise Speed
      243 km/h
      366 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
      1544 l
      2317 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6584 m
      9876 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2317 km
      3477 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1961 km
      2943 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
      4 min
      8 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      3 m
      6 m
    • Prop blade number
      3 qt
      5 qt
    • Guns
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      2 qt
      4 qt
    • Rockets
      9 qt
      15 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      120 qt
      182 qt
    • Price
      41 USD
      750000000 USD

Martin AM Mauler

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.6
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
46.1
925
Wingspan (Beam) (m)
0.1
 
15.2
95
Wing loading (kg/m2)
3.1
 
238
829
Rotors
Rotor number (qt)
1
 
4
8
Weights
Empty weight (kg)
8
 
6,920.5
276,800
Loaded weight (kg)
5
 
11,674.1
242,500
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
15
2,576
Speeds
Max. Speed (km/h)
25
 
537.5
28,165
Сruise Speed (km/h)
52
 
304.2
3,087
Fuel
Fuel Capacity (l)
23
 
1,930.6
320,000
Power
Total Power (hp)
0.4
 
3,000
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,230
161,544
Range (Ferry range) (km)
4
 
2,897
40,700
Сombat radius (km)
277
 
2,452.1
7,210
Dynamic Performance
Time to altitude (min)
0.6
 
5.9
105
to 3048 m
Propellers
Prop diameter (m)
1.8
 
4.3
5.8
Prop blade number (qt)
1
 
4
8
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) T-31 cannon
Missiles (qt)
1
 
3
24
Mark 13 torpedos
Rockets (qt)
1
 
12
76
Stat
Number built (qt)
0
 
151
43,000
Introduction 1944
First flight 26.08.1944
Stop production 1953

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