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    • Year
      1906
      2018
    • Length
      14 m
      22 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      52 m2
      79 m2
    • Wingspan (Beam)
      19 m
      30 m
    • Wing loading
      284 kg/m2
      426 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
      14587 kg
      21882 kg
    • Max. takeoff weight (Gross weight)
      20865 kg
      31298 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 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
      518 km/h
      778 km/h
    • Сruise Speed
      379 km/h
      569 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
      5624 l
      8436 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
      8160 hp
      12240 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8461 m
      12692 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2166 km
      3250 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      4 h
      8 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
      140800000 USD
      211200000 USD

Grumman E-2 Hawkeye

TypeAircraft
Company

Grumman Aerospace Corporation

Northrop Grumman

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
17.6
88.7
Height (m)
0.6
 
5.6
50.1
Wings
Wing area (m2)
1.1
 
65.0
925
Wingspan (Beam) (m)
0.1
 
24.6
95
Wing loading (kg/m2)
3.1
 
355
829
Weights
Empty weight (kg)
8
 
18,234.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
26,081.6
575,000
Capacity
Crew (per.)
1
 
5
112
Pilot, Copilot, Radar Officer (RO), Combat Information Center Officer (CICO), Aircraft Control Officer (ACO)
Speeds
Max. Speed (km/h)
25
 
648
28,165
Сruise Speed (km/h)
52
 
474
3,087
Fuel
Fuel Capacity (l)
23
 
7,030
320,000
Power
Total Power (hp)
0.4
 
10,200
60,000
2 powerplants 5100 hp each
Performance
Service ceiling (m)
0.6
 
10,576.6
161,544
Range (Ferry range) (km)
4
 
2,708
40,700
Endurance (h)
0.0
 
6
150
Stat
Price (USD)
41.5
 
176.0 million
750.0 million
Introduction 1960
First flight 21.10.1960

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