Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      29 m2
      44 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
      1143 kg
      1715 kg
    • Max. takeoff weight (Gross weight)
      2547 kg
      3822 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
      196 km/h
      294 km/h
    • Сruise Speed
      167 km/h
      251 km/h
    • Stall Speed
      82 km/h
      124 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      201 km/h
      303 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
      600 hp
      901 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3840 m
      5760 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      254 km
      383 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
      1 m/min
      36000 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
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Grumman G-164 Ag-Cat

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Biplane

Geometry
Length (m)
1.9
 
8.4
88.7
Height (m)
0.6
 
3.7
50.1
Wings
Wing area (m2)
1.1
 
36.5
925
Wingspan (Beam) (m)
0.1
 
12.9
95
Weights
Empty weight (kg)
8
 
1,428.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,184.2
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
245
28,165
Сruise Speed (km/h)
52
 
209
3,087
Stall Speed (km/h)
40
 
103
257.7
Never exceed speed (km/h)
108.0
 
252
1,050
Power
Total Power (hp)
0.4
 
750.7
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,800
161,544
Range (Ferry range) (km)
4
 
318.5
40,700
Stat
Introduction 1957
First flight 1957

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