Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      8 m
      13 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
      4305 kg
      6459 kg
    • Max. takeoff weight (Gross weight)
      8985 kg
      13479 kg
    • Loaded weight
      7292 kg
      10940 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
      832 km/h
      1250 km/h
    • Сruise Speed
      52 km/h
      3087 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
      0 hp
      60000 hp
    • Thrust
      30 kN
      46 kN
    • Service ceiling
      10241 m
      15362 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1352 km
      2028 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
      1402 m/min
      2104 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
      3 qt
      5 qt
    • Rockets
      4 qt
      8 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1113 qt
      1671 qt
    • Price
      41 USD
      750000000 USD

Grumman F-9 Cougar

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
12.9
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
10.5
95
Weights
Empty weight (kg)
8
 
5,382.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,232.3
575,000
Loaded weight (kg)
5
 
9,116
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
1,041
28,165
at 610 m
Power
Thrust (kN)
1.5
 
38
1,914
1 powerplant with water injection
Performance
Service ceiling (m)
0.6
 
12,801.6
161,544
Range (Ferry range) (km)
4
 
1,690
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,752.6
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) M3 cannon, 190 rounds per gun
Bombs (qt)
1
 
2
250
454 kg bombs
Missiles (qt)
1
 
4
24
AIM-9 Sidewinder air-to-air missiles
Rockets (qt)
1
 
6
76
5 in (127 mm) rockets
Stat
Number built (qt)
0
 
1,392
43,000
First flight 20.09.1951
Stop production 1974

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