Search filter

    • Year
      1906
      2018
    • Length
      10 m
      17 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      10 m
      16 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
      4611 kg
      6918 kg
    • Max. takeoff weight (Gross weight)
      8775 kg
      13164 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      824 km/h
      1236 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
      31 kN/kg
      47 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      22 kN
      34 kN
    • Service ceiling
      12533 m
      18801 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1040 km
      1560 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
      1944 m/min
      2916 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
      38 qt
      58 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      684 qt
      1026 qt
    • Price
      156998 USD
      235498 USD

Lockheed F-94 Starfire

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.6
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wingspan (Beam) (m)
0.1
 
12.9
95
Weights
Empty weight (kg)
8
 
5,764.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
10,969.7
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
1,030
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.5
2.1
Afterburning thrust (kN/kg)
29.4
 
38.9
980
1 powerplant
Thrust (kN)
1.5
 
28.2
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
15,666.7
161,544
Range (Ferry range) (km)
4
 
1,300
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,430
36,000
Combat
Rockets (qt)
1
 
48
76
24 or 48 × 2.75 in (70 mm) Mk 4/Mk 40 Folding-Fin Aerial Rockets
Stat
Number built (qt)
0
 
855
43,000
Price (USD)
41.5
 
196,248
750.0 million
Introduction 1949
First flight 16.04.1949
Stop production 1958

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