Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      5
      8
    • 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
      3055 kg
      4584 kg
    • Max. takeoff weight (Gross weight)
      6116 kg
      9175 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
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      772 km/h
      1158 km/h
    • Сruise Speed
      52 km/h
      3087 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      16 kN
      25 kN
    • Service ceiling
      11216 m
      16825 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1544 km
      2316 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
      1118 m/min
      1678 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
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      6 qt
      10 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1372 qt
      2058 qt
    • Price
      88000 USD
      132000 USD

Lockheed F-80 shooting Star

TypeAircraft
Company

Lockheed Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.5
88.7
Height (m)
0.6
 
3.4
50.1
Wings
Wing area (m2)
1.1
 
22.1
925
Wingspan (Beam) (m)
0.1
 
11.8
95
Aspect ratio
1.7
 
6.4
25.6
Weights
Empty weight (kg)
8
 
3,819.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,645.8
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
965
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
20.5
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
14,020.8
161,544
Range (Ferry range) (km)
4
 
1,930
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,398
36,000
Combat
Guns (qt)
1
 
6
18
0.50 in (12.7 mm) M3 Browning machine guns
Bombs (qt)
1
 
2
250
2 × 454 kg bombs
Rockets (qt)
1
 
8
76
127mm unguided rockets
Stat
Number built (qt)
0
 
1,715
43,000
Price (USD)
41.5
 
110,000
750.0 million
Introduction 1945
First flight 08.01.1944

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