Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      56 m2
    • Wingspan (Beam)
      17 m
      27 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
      6646 kg
      9970 kg
    • Max. takeoff weight (Gross weight)
      9488 kg
      14233 kg
    • Loaded weight
      8504 kg
      12756 kg
    • Crew
      3 per.
      5 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
      360 km/h
      540 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      192 km/h
      288 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
      1981 l
      2972 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
      2440 hp
      3660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5364 m
      8047 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1736 km
      2604 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1482 km
      2224 km
    • Endurance
      7 h
      11 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
      1027 qt
      1541 qt
    • Price
      41 USD
      750000000 USD

Grumman S-2 Tracker

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
13.3
88.7
Height (m)
0.6
 
5.3
50.1
Wings
Wing area (m2)
1.1
 
46.1
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Weights
Empty weight (kg)
8
 
8,307.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
11,860.1
575,000
Loaded weight (kg)
5
 
10,630
242,500
Capacity
Crew (per.)
1
 
4
112
two pilots, two detection systems operators
Speeds
Ground Speed (km/h)
96.6
 
450
1,500
Сruise Speed (km/h)
52
 
240
3,087
Fuel
Fuel Capacity (l)
23
 
2,476.3
320,000
Power
Total Power (hp)
0.4
 
3,050
60,000
2 powerplants 1525hp each
Performance
Service ceiling (m)
0.6
 
6,705.6
161,544
Range (Ferry range) (km)
4
 
2,170
40,700
Сombat radius (km)
277
 
1,853
7,210
Endurance (h)
0.0
 
9
150
Stat
Number built (qt)
0
 
1,284
43,000
Introduction 1954
First flight 04.12.1952

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