Search filter

    • Year
      1906
      2018
    • Length
      17 m
      27 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      64 m2
      97 m2
    • Wingspan (Beam)
      22 m
      35 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
      9103 kg
      13655 kg
    • Max. takeoff weight (Gross weight)
      14478 kg
      21719 kg
    • Loaded weight
      5 kg
      242500 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
      248 km/h
      374 km/h
    • Сruise Speed
      228 km/h
      344 km/h
    • Stall Speed
      97 km/h
      147 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
      4088 l
      6132 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
      2880 hp
      4320 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8046 m
      12070 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      817 km
      1227 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
      528 m/min
      792 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      3 qt
    • Prop diameter
      3 m
      5 m
    • Prop blade number
      2 qt
      4 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
      37 qt
      57 qt
    • Price
      41 USD
      750000000 USD

Martin 2-0-2

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
21.7
88.7
Height (m)
0.6
 
8.7
50.1
Wings
Wing area (m2)
1.1
 
80.3
925
Wingspan (Beam) (m)
0.1
 
28.4
95
Weights
Empty weight (kg)
8
 
11,378.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
18,098.3
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
311
28,165
at 4300 m
Сruise Speed (km/h)
52
 
286
3,087
at 3700 m
Stall Speed (km/h)
40
 
122.3
257.7
Fuel
Fuel Capacity (l)
23
 
5,110
320,000
Power
Total Power (hp)
0.4
 
3,600
60,000
2 powerplants 1800 hp each
Performance
Service ceiling (m)
0.6
 
10,058
161,544
Range (Ferry range) (km)
4
 
1,022
40,700
36 passengers, baggage and 450 kg cargo, reserves for 320 km plus 45 minutes
Dynamic Performance
Rate of climb (m/min)
1.9
 
660
36,000
Propellers
Propellers (qt)
1
 
2
8
Prop diameter (m)
1.8
 
4.0
5.8
Prop blade number (qt)
1
 
3
8
Stat
Number built (qt)
0
 
47
43,000
Introduction 1946
First flight 22.11.1946
Stop production 1975

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