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    • Year
      1906
      2018
    • Length
      13 m
      20 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      14 m2
      22 m2
    • Wingspan (Beam)
      5 m
      8 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
      5080 kg
      7620 kg
    • Max. takeoff weight (Gross weight)
      10536 kg
      15804 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      5 qt
      9 qt
    • Ground Speed
      1178 km/h
      1500 km/h
    • Max. Speed
      1738 km/h
      2608 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      216 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
      2120 l
      3180 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
      55 kN/kg
      83 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      38 kN
      58 kN
    • Service ceiling
      12000 m
      18000 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1094 km
      1642 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
      5 G
      9 G
    • Rate of climb
      11712 m/min
      17568 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
      2 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      3 qt
      5 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
      2062 qt
      3094 qt
    • Price
      1136000 USD
      1704000 USD

Lockheed F-104 Starfighter

TypeAircraft
Company

Lockheed Corporation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
16.7
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
18.2
925
Wingspan (Beam) (m)
0.1
 
6.4
95
Weights
Empty weight (kg)
8
 
6,350
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,170
575,000
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
7
2,576
with a capacity of 1814 kg
Speeds
Ground Speed (km/h)
96.6
 
1,473
1,500
Max. Speed (km/h)
25
 
2,173
28,165
Landing Speed (km/h)
68
 
270
270
Fuel
Fuel Capacity (l)
23
 
2,650
320,000
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Afterburning thrust (kN/kg)
29.4
 
69
980
1 powerplant
Thrust (kN)
1.5
 
48
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
15,000
161,544
Range (Ferry range) (km)
4
 
1,368
40,700
Dynamic Performance
Load factor from (G)
2
 
7
9
Rate of climb (m/min)
1.9
 
14,640
36,000
Combat
Guns (qt)
1
 
1
18
20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, 725 rounds
Missiles (qt)
1
 
4
24
AIM-9 Sidewinder
Stat
Number built (qt)
0
 
2,578
43,000
Price (USD)
41.5
 
1.4 million
750.0 million
Introduction 20.02.1958
First flight 17.02.1956
Stop production 31.10.2004

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