Search filter

    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      33 m2
      51 m2
    • Wingspan (Beam)
      12 m
      19 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
      5903 kg
      8856 kg
    • Max. takeoff weight (Gross weight)
      9333 kg
      14000 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
      592 km/h
      888 km/h
    • Сruise Speed
      280 km/h
      420 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
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3360 hp
      5040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9851 m
      14777 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1520 km
      2280 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
      1104 m/min
      1657 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
      6 qt
      10 qt
    • Bombs
      1 qt
      3 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      2 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      291 qt
      437 qt
    • Price
      41 USD
      750000000 USD

Grumman F7F Tigercat

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
13.8
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
42.3
925
Wingspan (Beam) (m)
0.1
 
15.7
95
Weights
Empty weight (kg)
8
 
7,380.0
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,666.4
575,000
Capacity
Crew (per.)
1
 
2
112
pilot, radar operator
Speeds
Max. Speed (km/h)
25
 
740
28,165
Сruise Speed (km/h)
52
 
350
3,087
Power
Total Power (hp)
0.4
 
4,200
60,000
2 powerplant 2100 hp each
Performance
Service ceiling (m)
0.6
 
12,313.9
161,544
Range (Ferry range) (km)
4
 
1,900
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,380.7
36,000
Combat
Guns (qt)
1
 
8
18
4 × 20 mm (0.79 in) M2 cannon; 4 × 0.50 in (12.7 mm) M2 Browning machine gun
Bombs (qt)
1
 
2
250
454 kg bombs under wings or
Torpedoes (qt)
1
 
1
4
torpedo under fuselage
Stat
Number built (qt)
0
 
364
43,000
Introduction 1943
First flight 02.11.1943
Stop production 1954

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