Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      28 m2
      43 m2
    • Wingspan (Beam)
      9 m
      15 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
      480 kg
      720 kg
    • Max. takeoff weight (Gross weight)
      624 kg
      936 kg
    • Loaded weight
      624 kg
      936 kg
    • Crew
      1 per.
      3 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
      121 km/h
      183 km/h
    • Сruise Speed
      100 km/h
      150 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
      72 hp
      108 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2320 m
      3480 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 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
      13 qt
      21 qt
    • Price
      41 USD
      750000000 USD

Martin T

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.0
88.7
Height (m)
0.6
 
2.9
50.1
Wings
Wing area (m2)
1.1
 
35.2
925
Wingspan (Beam) (m)
0.1
 
11.8
95
Weights
Empty weight (kg)
8
 
600
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
780
575,000
Loaded weight (kg)
5
 
780
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and instructor
Speeds
Max. Speed (km/h)
25
 
152
28,165
Сruise Speed (km/h)
52
 
125
3,087
Power
Total Power (hp)
0.4
 
90
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
2,900
161,544
Stat
Number built (qt)
0
 
17
43,000
Introduction 1913
First flight 1913

Similar aircraft

Get more

Comments