Search filter

    • Year
      1906
      2018
    • Length
      19 m
      30 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      60 m2
      91 m2
    • Wingspan (Beam)
      16 m
      26 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
      13 kg
      20 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      23768 kg
      35654 kg
    • Crew
      1 per.
      3 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
      748 km/h
      1124 km/h
    • Сruise Speed
      622 km/h
      934 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
      81 kN
      123 kN
    • Service ceiling
      10972 m
      16458 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5308 km
      7962 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
      206 qt
      310 qt
    • Price
      41 USD
      750000000 USD

Grumman Gulfstream II

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
24.4
88.7
Height (m)
0.6
 
7.5
50.1
Wings
Wing area (m2)
1.1
 
75.2
925
Wingspan (Beam) (m)
0.1
 
21.0
95
Weights
Empty weight (kg)
8
 
16.6
276,800
Loaded weight (kg)
5
 
29,711
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
936
28,165
Сruise Speed (km/h)
52
 
778
3,087
Power
Thrust (kN)
1.5
 
102
1,914
2 powerplants 51 kN each
Performance
Service ceiling (m)
0.6
 
13,715
161,544
Range (Ferry range) (km)
4
 
6,635
40,700
Stat
Number built (qt)
0
 
258
43,000
Introduction 1966
First flight 02.10.1966

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