Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 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
      303 kg/m2
      455 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
      12245 kg
      18369 kg
    • Max. takeoff weight (Gross weight)
      21772 kg
      32659 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      7480 kg
      11220 kg
    • Payload
      3628 kg
      5444 kg
    • Capacity passengers
      20 per.
      32 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      508 km/h
      762 km/h
    • Сruise Speed
      372 km/h
      558 km/h
    • Stall Speed
      121 km/h
      183 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
      9939 l
      14909 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
      7360 hp
      11040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8168 m
      12253 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1926 km
      2890 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
      902 m/min
      1354 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
      46 qt
      70 qt
    • Price
      31168000 USD
      46752000 USD

Grumman C-2 Greyhound

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
17.3
88.7
Height (m)
0.6
 
4.9
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
 
378.9
829
Weights
Empty weight (kg)
8
 
15,306.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
27,215.5
575,000
Capacity
Crew (per.)
1
 
4
112
2 pilots, 2 aircrew
Useful load (kg)
26.4
 
9,350
90,700
Payload (kg)
23
 
4,535.9
122,470
Capacity passengers (per.)
1
 
26
400
26 passengers, 12 litter patients
Speeds
Max. Speed (km/h)
25
 
635
28,165
at 3660 m
Сruise Speed (km/h)
52
 
465
3,087
at 8750 m
Stall Speed (km/h)
40
 
152
257.7
at idle power
Fuel
Fuel Capacity (l)
23
 
12,424
320,000
6905 l + optional 5519 l
Power
Total Power (hp)
0.4
 
9,200
60,000
2 powerplants 4600 hp
Performance
Service ceiling (m)
0.6
 
10,210.8
161,544
Range (Ferry range) (km)
4
 
2,407.6
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,127.8
36,000
Stat
Number built (qt)
0
 
58
43,000
Price (USD)
41.5
 
39.0 million
750.0 million
Introduction 1964
First flight 18.11.1964
Stop production 1987

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