Search filter

    • Year
      1906
      2018
    • Length
      41 m
      62 m
    • Height
      9 m
      15 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      240 m2
      360 m2
    • Wingspan (Beam)
      39 m
      59 m
    • Wing loading
      392 kg/m2
      588 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
      52432 kg
      78649 kg
    • Max. takeoff weight (Gross weight)
      117600 kg
      176400 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      9 per.
      15 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
      729 km/h
      1095 km/h
    • Сruise Speed
      636 km/h
      956 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
      55720 l
      83580 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
      288 kN
      433 kN
    • Service ceiling
      10000 m
      15000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3778 km
      5668 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
      633 m/min
      951 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
      18 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
      228 qt
      342 qt
    • Price
      41 USD
      750000000 USD

Lockheed C-141 Starlifter

TypeAircraft
Company

Lockheed Corporation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
51.3
88.7
Height (m)
0.6
 
12
50.1
Wings
Wing area (m2)
1.1
 
300
925
Wingspan (Beam) (m)
0.1
 
48.8
95
Wing loading (kg/m2)
3.1
 
490
829
Weights
Empty weight (kg)
8
 
65,540.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
147,000
575,000
Capacity
Crew (per.)
1
 
12
112
including 5 medical crew on medevac flights
Speeds
Max. Speed (km/h)
25
 
912
28,165
Сruise Speed (km/h)
52
 
796
3,087
Fuel
Fuel Capacity (l)
23
 
69,650
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.3
2.1
Thrust (kN)
1.5
 
360.4
1,914
4 powerplants 90,1 kN each
Performance
Service ceiling (m)
0.6
 
12,500
161,544
Range (Ferry range) (km)
4
 
4,723
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
792
36,000
Stat
Number built (qt)
0
 
285
43,000
Introduction 1963
First flight 17.12.1963
Stop production 06.05.2006

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