Search filter

    • Year
      1906
      2018
    • Length
      11 m
      18 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      61 m2
    • Wingspan (Beam)
      14 m
      23 m
    • Wing loading
      180 kg/m2
      272 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
      5802 kg
      8705 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      8720 kg
      13080 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
      390 km/h
      586 km/h
    • Сruise Speed
      289 km/h
      435 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
      2720 hp
      4080 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5680 m
      8520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1261 km
      1893 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
      11 qt
      17 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      728 kg
      1092 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1260 qt
      1890 qt
    • Price
      96000 USD
      144000 USD

Martin 187 Baltimore

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
14.8
88.7
Height (m)
0.6
 
4.3
50.1
Wings
Wing area (m2)
1.1
 
50.0
925
Wingspan (Beam) (m)
0.1
 
18.7
95
Wing loading (kg/m2)
3.1
 
226
829
Weights
Empty weight (kg)
8
 
7,253.4
276,800
Loaded weight (kg)
5
 
10,900
242,500
Capacity
Crew (per.)
1
 
4
112
pilot, navigator/bombardier, radio operator, gunner
Speeds
Max. Speed (km/h)
25
 
488
28,165
at 3540 m
Сruise Speed (km/h)
52
 
362
3,087
Power
Total Power (hp)
0.4
 
3,400
60,000
Performance
Service ceiling (m)
0.6
 
7,100
161,544
Range (Ferry range) (km)
4
 
1,577
40,700
Combat
Guns (qt)
1
 
14
18
4 × wing mounted 0.303 in (7.7 mm) M1919 Browning machine guns. 2–4 × 0.303 in (7.7 mm) machine guns in dorsal turret, 2 × 0.303 in (7.7 mm) machine guns in ventral position and provisions for up to 4 × fixed rear firing 0.303 in (7.7 mm) machine guns.
Bombs weight (kg)
2
 
910
39,000
carried internally
Stat
Number built (qt)
0
 
1,575
43,000
Price (USD)
41.5
 
120,000
750.0 million
Introduction 1941
First flight 14.06.1941
Stop production 1949

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