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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      19 m2
      29 m2
    • Wingspan (Beam)
      7 m
      12 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
      1192 kg
      1789 kg
    • Max. takeoff weight (Gross weight)
      1739 kg
      2610 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
      340 km/h
      510 km/h
    • Сruise Speed
      192 km/h
      290 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
      760 hp
      1140 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8095 m
      12144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1280 km
      1920 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
      682 m/min
      1025 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
      3 qt
    • Bombs
      1 qt
      3 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
      117 qt
      177 qt
    • Price
      16339 USD
      24509 USD

Grumman F3F

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Biplane

Geometry
Length (m)
1.9
 
7.1
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
24.2
925
Wingspan (Beam) (m)
0.1
 
9.8
95
Weights
Empty weight (kg)
8
 
1,490.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,175.0
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
425
28,165
at 4658 m
Сruise Speed (km/h)
52
 
241
3,087
Power
Total Power (hp)
0.4
 
950
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
10,119.4
161,544
Range (Ferry range) (km)
4
 
1,600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
853.4
36,000
Combat
Guns (qt)
1
 
2
18
1× 0.30 in (7.62 mm) M1919 machine gun, 500 rounds (left); 1× 0.50 in (12.7 mm) M2 machine gun, 200 rounds (right)
Bombs (qt)
1
 
2
250
52.6 kg Mk IV bombs, one under each wing
Stat
Number built (qt)
0
 
147
43,000
Price (USD)
41.5
 
20,424
750.0 million
Introduction 1935
First flight 20.03.1935
Stop production 01.11.1943

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