Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      45 m2
      69 m2
    • Wingspan (Beam)
      16 m
      25 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
      7068 kg
      10604 kg
    • Max. takeoff weight (Gross weight)
      12728 kg
      19092 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      8 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
      350 km/h
      526 km/h
    • Сruise Speed
      296 km/h
      444 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
      5900 m
      8852 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1739 km
      2609 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
      264 m/min
      396 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
      14 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      6 qt
      10 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      1088 kg
      1632 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      7852 qt
      11780 qt
    • Price
      41 USD
      750000000 USD

North American Aviation B-25 Mitchell

TypeAircraft
Company

North American Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16.1
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
56.7
925
Wingspan (Beam) (m)
0.1
 
20.6
95
Weights
Empty weight (kg)
8
 
8,836.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,910
575,000
Capacity
Crew (per.)
1
 
6
112
one pilot, one co-pilot, navigator/bombardier, turret gunner/engineer, radio operator/waist gunner, tail gunner
Speeds
Max. Speed (km/h)
25
 
438
28,165
at 3960 m
Сruise Speed (km/h)
52
 
370
3,087
Power
Total Power (hp)
0.4
 
3,400
60,000
2 powerplants 1700 hp each
Performance
Service ceiling (m)
0.6
 
7,376.2
161,544
Range (Ferry range) (km)
4
 
2,174
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
330
36,000
Combat
Guns (qt)
1
 
18
18
12.7 mm machine guns and 75 mm (2.95 in) T13E1 cannon
Rockets (qt)
1
 
8
76
1
 
8
76
127 mm high velocity aircraft rockets (HVAR)
Torpedoes (qt)
1
 
1
4
external Mark 13 torpedo
Bombs weight (kg)
2
 
1,360
39,000
Stat
Number built (qt)
0
 
9,816
43,000
Introduction 1941
First flight 19.08.1940
Stop production 1979

Similar aircraft

Get more

Museums on map

Museums

Comments