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    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      7 m2
      11 m2
    • Wingspan (Beam)
      5 m
      9 m
    • Wing loading
      58 kg/m2
      88 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
      369 kg
      555 kg
    • Max. takeoff weight (Gross weight)
      544 kg
      817 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
      1 per.
      2 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      177 km/h
      267 km/h
    • Сruise Speed
      166 km/h
      250 km/h
    • Stall Speed
      77 km/h
      117 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
      86 hp
      130 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3352 m
      5030 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      628 km
      942 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
      186 m/min
      280 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
      544 qt
      816 qt
    • Price
      5196 USD
      7794 USD

Grumman American AA-1B Trainer

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
5.9
88.7
Height (m)
0.6
 
2.1
50.1
Wings
Wing area (m2)
1.1
 
9.1
925
Wingspan (Beam) (m)
0.1
 
7.5
95
Wing loading (kg/m2)
3.1
 
72.8
829
Weights
Empty weight (kg)
8
 
461.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
680.4
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
1
400
Speeds
Max. Speed (km/h)
25
 
222
28,165
Сruise Speed (km/h)
52
 
208
3,087
Stall Speed (km/h)
40
 
97
257.7
Power
Total Power (hp)
0.4
 
108
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,191
161,544
Range (Ferry range) (km)
4
 
785
40,700
at 2438 m
Dynamic Performance
Rate of climb (m/min)
1.9
 
233.2
36,000
Stat
Number built (qt)
0
 
680
43,000
680 AA-1Bs were produced by Grumman American
Price (USD)
41.5
 
6,495
750.0 million
Introduction 1963
First flight 1963

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