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    • Year
      1906
      2018
    • Length
      5 m
      8 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      26 m2
    • Wingspan (Beam)
      6 m
      11 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
      976 kg
      1465 kg
    • Max. takeoff weight (Gross weight)
      1395 kg
      2094 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
      297 km/h
      447 km/h
    • Сruise Speed
      180 km/h
      270 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
      560 hp
      840 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6608 m
      9913 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1268 km
      1902 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
      499 m/min
      750 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
      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
      44 qt
      66 qt
    • Price
      9600 USD
      14400 USD

Grumman F2F

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Biplane

Geometry
Length (m)
1.9
 
6.5
88.7
Height (m)
0.6
 
2.8
50.1
Wings
Wing area (m2)
1.1
 
21.4
925
Wingspan (Beam) (m)
0.1
 
8.7
95
Weights
Empty weight (kg)
8
 
1,220.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,745.0
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
372
28,165
Сruise Speed (km/h)
52
 
225
3,087
Power
Total Power (hp)
0.4
 
700
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,260.1
161,544
Range (Ferry range) (km)
4
 
1,585
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
624.8
36,000
Combat
Guns (qt)
1
 
2
18
.30-in machine guns
Stat
Number built (qt)
0
 
55
43,000
Price (USD)
41.5
 
12,000
750.0 million
Introduction 1933
First flight 18.10.1933
Stop production 1940

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