Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      40 m2
      62 m2
    • Wingspan (Beam)
      16 m
      24 m
    • Wing loading
      220 kg/m2
      330 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
      7328 kg
      10992 kg
    • Max. takeoff weight (Gross weight)
      12000 kg
      18000 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
      257 km/h
      387 km/h
    • Сruise Speed
      184 km/h
      276 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
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6416 m
      9624 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2136 km
      3204 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
      739 m/min
      1109 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
      4 qt
      8 qt
    • Bombs
      4 qt
      8 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1120 kg
      1680 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Lockheed B-34 Lexington

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
15.7
88.7
Height (m)
0.6
 
3.6
50.1
Wings
Wing area (m2)
1.1
 
51.2
925
Wingspan (Beam) (m)
0.1
 
20
95
Wing loading (kg/m2)
3.1
 
275
829
Weights
Empty weight (kg)
8
 
9,160
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,000
575,000
Capacity
Crew (per.)
1
 
6
112
Speeds
Max. Speed (km/h)
25
 
322
28,165
Сruise Speed (km/h)
52
 
230
3,087
Power
Total Power (hp)
0.4
 
4,000
60,000
2 powerplants 2000 hp each
Performance
Service ceiling (m)
0.6
 
8,020
161,544
Range (Ferry range) (km)
4
 
2,670
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
924
36,000
Combat
Guns (qt)
1
 
6
18
4 × .50 BMG (12.7 mm) Browning M2 machine guns; 2 × .30 cal. (7.62 mm) M1919 Browning machine guns
Bombs (qt)
1
 
1
250
torpedo or
1
 
6
250
depth charges or
Bombs weight (kg)
2
 
1,400
39,000
general ordnance
Stat
Introduction 1941
First flight 31.07.1941

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