Search filter

    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      22 m2
      34 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
      2941 kg
      4413 kg
    • Max. takeoff weight (Gross weight)
      4360 kg
      6540 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
      492 km/h
      740 km/h
    • Сruise Speed
      269 km/h
      405 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
      1920 hp
      2880 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8800 m
      13200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1440 km
      2160 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
      975 m/min
      1464 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
      3 qt
      5 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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Grumman XF5F Skyrocket

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
8.8
88.7
Height (m)
0.6
 
3.5
50.1
Wings
Wing area (m2)
1.1
 
28.2
925
Wingspan (Beam) (m)
0.1
 
12.8
95
Weights
Empty weight (kg)
8
 
3,677.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,450
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
616
28,165
Сruise Speed (km/h)
52
 
337
3,087
Power
Total Power (hp)
0.4
 
2,400
60,000
2 powerplants 1200 hp each
Performance
Service ceiling (m)
0.6
 
11,000
161,544
Range (Ferry range) (km)
4
 
1,800
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,219.2
36,000
Combat
Guns (qt)
1
 
4
18
2 × 0.5 in (12.7 mm) machine guns; 2 x 0.3 in (7.62mm) machine guns
Bombs (qt)
1
 
2
250
75 kg bombs
Stat
Number built (qt)
0
 
1
43,000
Introduction 1940
First flight 01.04.1940
Stop production 11.12.1944

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