Search filter

    • Year
      1906
      2018
    • Length
      22 m
      34 m
    • Height
      6 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      159 m2
      239 m2
    • Wingspan (Beam)
      31 m
      48 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
      9203 kg
      13805 kg
    • Max. takeoff weight (Gross weight)
      18960 kg
      28442 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      7 per.
      11 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
      232 km/h
      348 km/h
    • Сruise Speed
      167 km/h
      251 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
      3040 hp
      4560 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2438 m
      3658 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4120 km
      6180 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
      2 qt
      4 qt
    • Price
      41 USD
      750000000 USD

Martin M-130 Clipper

TypeAircraft
Company

Glenn L. Martin Company

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
27.7
88.7
Height (m)
0.6
 
7.5
50.1
Wings
Wing area (m2)
1.1
 
199
925
Wingspan (Beam) (m)
0.1
 
39.7
95
Weights
Empty weight (kg)
8
 
11,504
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
23,701.1
575,000
Capacity
Crew (per.)
1
 
9
112
Captain, First Officer, Junior Flight Officer, Engineering Officer, Assistant Engineering Officer, Radio Operator, Navigation Officer, plus cabin stewards
Speeds
Max. Speed (km/h)
25
 
290
28,165
Сruise Speed (km/h)
52
 
209
3,087
Power
Total Power (hp)
0.4
 
3,800
60,000
4 powerplants 950 hp each, 830 hp each n the beginning
Performance
Service ceiling (m)
0.6
 
3,048
161,544
Range (Ferry range) (km)
4
 
5,150
40,700
Stat
Number built (qt)
0
 
3
43,000
Introduction 1934
First flight 30.12.1934

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