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    • Year
      1906
      2018
    • Length
      11 m
      17 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      36 m2
      55 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
      7504 kg
      11258 kg
    • Max. takeoff weight (Gross weight)
      9652 kg
      14479 kg
    • Loaded weight
      9018 kg
      13528 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
      96 km/h
      1500 km/h
    • Max. Speed
      306 km/h
      460 km/h
    • Сruise Speed
      210 km/h
      316 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
      2440 hp
      3660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3852 m
      5780 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1332 km
      2000 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      5 h
      9 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
      273 m/min
      410 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
      70 qt
      106 qt
    • Price
      41 USD
      750000000 USD

Grumman E-1 Tracer

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
13.8
88.7
Height (m)
0.6
 
5.1
50.1
Wings
Wing area (m2)
1.1
 
45.1
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Weights
Empty weight (kg)
8
 
9,381
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
12,065.6
575,000
Loaded weight (kg)
5
 
11,273
242,500
Capacity
Crew (per.)
1
 
4
112
two pilots, two RADAR/Intercept Controllers
Speeds
Max. Speed (km/h)
25
 
383
28,165
at 1220 m
Сruise Speed (km/h)
52
 
263
3,087
Power
Total Power (hp)
0.4
 
3,050
60,000
2 powerplants 1525 hp each
Performance
Service ceiling (m)
0.6
 
4,815.8
161,544
Range (Ferry range) (km)
4
 
1,666
40,700
Endurance (h)
0.0
 
6.8
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
341.4
36,000
Stat
Number built (qt)
0
 
88
43,000
Introduction 1956
First flight 17.12.1956
Stop production 1977

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