Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      21 m2
    • Wingspan (Beam)
      8 m
      14 m
    • Wing loading
      80 kg/m2
      121 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
      932 kg
      1399 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      1378 kg
      2069 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      248 km/h
      374 km/h
    • Сruise Speed
      236 km/h
      356 km/h
    • Stall Speed
      93 km/h
      141 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      90 km/h
      113 km/h
    • Never exceed speed
      278 km/h
      418 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      1 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      256 hp
      384 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4240 m
      6360 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1733 km
      2601 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
      280 m/min
      421 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
      18 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
      92 qt
      138 qt
    • Price
      41 USD
      750000000 USD

Grumman American GA-7 Cougar

TypeAircraft
Company

Grumman Aerospace Corporation

Gulfstream Aerospace Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.7
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
17.1
925
Wingspan (Beam) (m)
0.1
 
11.2
95
Wing loading (kg/m2)
3.1
 
100.8
829
Weights
Empty weight (kg)
8
 
1,165.3
276,800
Loaded weight (kg)
5
 
1,723.7
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
311
28,165
Сruise Speed (km/h)
52
 
296
3,087
true airspeed
Stall Speed (km/h)
40
 
117
257.7
calibrated airspeed, flaps down
Minimum control speed (km/h)
24
 
113
113
indicated airspeed
Never exceed speed (km/h)
108.0
 
348
1,050
Power
Power/mass (hp/kg)
0.0
 
0.2
22.1
Total Power (hp)
0.4
 
320
60,000
2 powerplants 160 hp each
Performance
Service ceiling (m)
0.6
 
5,300
161,544
Range (Ferry range) (km)
4
 
2,167
40,700
maximum economy with no reserves
Dynamic Performance
Rate of climb (m/min)
1.9
 
350.5
36,000
Stat
Number built (qt)
0
 
115
43,000
Introduction 1974
First flight 20.12.1974

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