Search filter

    • Year
      1906
      2018
    • Length
      8 m
      13 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      25 m2
      39 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      147 kg/m2
      221 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      4
      7
    • 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
      3352 kg
      5029 kg
    • Max. takeoff weight (Gross weight)
      5593 kg
      8391 kg
    • Loaded weight
      4571 kg
      6857 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
      496 km/h
      746 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      108 km/h
      162 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
      1211 l
      1817 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
      1760 hp
      2640 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9095 m
      13643 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1968 km
      2952 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
      853 m/min
      1281 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      3 m
      5 m
    • Prop blade number
      2 qt
      4 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
      9820 qt
      14730 qt
    • Price
      28000 USD
      42000 USD

Grumman F6F Hellcat

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
10.2
88.7
Height (m)
0.6
 
4.0
50.1
Wings
Wing area (m2)
1.1
 
32.0
925
Wingspan (Beam) (m)
0.1
 
13.1
95
Wing loading (kg/m2)
3.1
 
184
829
Aspect ratio
1.7
 
5.5
25.6
Weights
Empty weight (kg)
8
 
4,190.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,992.1
575,000
Loaded weight (kg)
5
 
5,714
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
621
28,165
Stall Speed (km/h)
40
 
135
257.7
Fuel
Fuel Capacity (l)
23
 
1,514
320,000
946 L internal + 568 L external drop tanks
Power
Total Power (hp)
0.4
 
2,200
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
11,369.0
161,544
Range (Ferry range) (km)
4
 
2,460
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,066.8
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
4
5.8
Prop blade number (qt)
1
 
3
8
Stat
Number built (qt)
0
 
12,275
43,000
Price (USD)
41.5
 
35,000
750.0 million
Introduction 1942
First flight 26.06.1942
Stop production 1960

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