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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      16 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      66 kg/m2
      100 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
      544 kg
      817 kg
    • Max. takeoff weight (Gross weight)
      870 kg
      1307 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      212 km/h
      318 km/h
    • Сruise Speed
      184 km/h
      276 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
      144 hp
      216 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3364 m
      5048 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1016 km
      1525 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
      207 m/min
      311 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
      2625 qt
      3939 qt
    • Price
      41 USD
      750000000 USD

Grumman American AA-5 Traveler

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
6.7
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
13
925
Wingspan (Beam) (m)
0.1
 
9.6
95
Wing loading (kg/m2)
3.1
 
83
829
Weights
Empty weight (kg)
8
 
680.4
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,088.6
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
265
28,165
Сruise Speed (km/h)
52
 
230
3,087
Power
Total Power (hp)
0.4
 
180
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,206.2
161,544
Range (Ferry range) (km)
4
 
1,270.5
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
259.1
36,000
Stat
Number built (qt)
0
 
3,282
43,000
Introduction 1970
First flight 21.08.1970

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