Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      50 m2
      76 m2
    • Wingspan (Beam)
      17 m
      26 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
      3512 kg
      5270 kg
    • Max. takeoff weight (Gross weight)
      5951 kg
      8927 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      170 km/h
      256 km/h
    • Сruise Speed
      248 km/h
      374 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
      1240 hp
      1860 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5900 m
      8852 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1596 km
      2396 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
      336 m/min
      505 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
      2 qt
      4 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
      96 qt
      146 qt
    • Price
      41666 USD
      62500 USD

Martin B-10

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
13.6
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
63
925
Wingspan (Beam) (m)
0.1
 
21.5
95
Weights
Empty weight (kg)
8
 
4,391.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,438.9
575,000
Capacity
Crew (per.)
1
 
4
112
pilot, co-pilot/radio operator, bombardier/gunner, gunner
Speeds
Max. Speed (km/h)
25
 
213
28,165
Сruise Speed (km/h)
52
 
311
3,087
1 powerplant
Power
Total Power (hp)
0.4
 
1,550
60,000
2 powerplants
Performance
Service ceiling (m)
0.6
 
7,376.2
161,544
Range (Ferry range) (km)
4
 
1,996
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
420.6
36,000
Combat
Guns (qt)
1
 
3
18
.30 in (7.62mm) Browning machine guns in nose, dorsal, and belly positions
Stat
Number built (qt)
0
 
121
43,000
Price (USD)
41.5
 
52,083
750.0 million
Introduction 1932
First flight 16.02.1932
Stop production 1949

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