Search filter

    • Year
      1906
      2018
    • Length
      32 m
      50 m
    • Height
      8 m
      13 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      141 m2
      213 m2
    • Wingspan (Beam)
      25 m
      38 m
    • Wing loading
      248 kg/m2
      372 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
      35358 kg
      53038 kg
    • Max. takeoff weight (Gross weight)
      64010 kg
      96017 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      31512 kg
      47268 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
      883 km/h
      1325 km/h
    • Сruise Speed
      688 km/h
      1034 km/h
    • Stall Speed
      196 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      248 kN
      374 kN
    • Service ceiling
      12192 m
      18288 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2518 km
      3779 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1111 km
      1667 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
      3 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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

Martin P6M SeaMaster

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
40.9
88.7
Height (m)
0.6
 
10.3
50.1
Wings
Wing area (m2)
1.1
 
177
925
Wingspan (Beam) (m)
0.1
 
31.3
95
Wing loading (kg/m2)
3.1
 
310
829
Weights
Empty weight (kg)
8
 
44,198
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
80,013.7
575,000
Capacity
Crew (per.)
1
 
4
112
Useful load (kg)
26.4
 
39,390
90,700
Speeds
Max. Speed (km/h)
25
 
1,104
28,165
Сruise Speed (km/h)
52
 
861
3,087
Stall Speed (km/h)
40
 
245
257.7
Power off, flaps down, T.O. wt
Power
Thrust/weight (kN/kg)
0.0
 
0.6
2.1
Thrust (kN)
1.5
 
311.2
1,914
4 powerplants 77,8 kN each
Performance
Service ceiling (m)
0.6
 
15,240
161,544
Range (Ferry range) (km)
4
 
3,148.4
40,700
Сombat radius (km)
277
 
1,389
7,210
carrying 13,608 kg payload
Combat
Guns (qt)
1
 
2
18
20 mm cannon in rear remote operated turret
Stat
Number built (qt)
0
 
12
43,000
Introduction 1955
First flight 14.07.1955

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