Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      65 m2
      99 m2
    • Wingspan (Beam)
      13 m
      21 m
    • Wing loading
      42 kg/m2
      64 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
      2109 kg
      3165 kg
    • Max. takeoff weight (Gross weight)
      3456 kg
      5184 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      140 km/h
      210 km/h
    • Сruise Speed
      116 km/h
      174 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
      616 hp
      924 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      1926 m
      2890 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      816 km
      1224 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
      72 m/min
      110 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      13 min
      21 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
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      99 qt
      149 qt
    • Price
      41 USD
      750000000 USD

Martin T3M

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
12.6
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
82.1
925
Wingspan (Beam) (m)
0.1
 
17.3
95
Wing loading (kg/m2)
3.1
 
52.6
829
Weights
Empty weight (kg)
8
 
2,637.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,320
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
175
28,165
Сruise Speed (km/h)
52
 
145
3,087
Power
Total Power (hp)
0.4
 
770
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
2,407.9
161,544
Range (Ferry range) (km)
4
 
1,020
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
91
36,000
Time to altitude (min)
0.6
 
16.8
105
to 3050 m
Combat
Guns (qt)
1
 
1
18
flexibly mounted 0.3 in (7.62 mm) machine gun in rear cockpit
Torpedoes (qt)
1
 
1
4
torpedo or bombs under fuselage
Stat
Number built (qt)
0
 
124
43,000
Introduction 1926
First flight 1926
Stop production 1932

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