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    • Year
      1906
      2018
    • Length
      17 m
      26 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      62 m2
      94 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      219 kg/m2
      329 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
      12827 kg
      19242 kg
    • Max. takeoff weight (Gross weight)
      22207 kg
      33312 kg
    • Loaded weight
      17015 kg
      25523 kg
    • Crew
      2 per.
      4 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
      580 km/h
      872 km/h
    • Сruise Speed
      512 km/h
      768 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
      7968 l
      11954 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
      8056 hp
      12084 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      9144 m
      13716 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2806 km
      4210 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
      1662 m/min
      2495 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
      3 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      3810 kg
      5716 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

North American Aviation XA2J Super Savage

TypeAircraft
Company

North American Aviation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
21.4
88.7
Height (m)
0.6
 
7.4
50.1
Wings
Wing area (m2)
1.1
 
77.8
925
Wingspan (Beam) (m)
0.1
 
21.8
95
Wing loading (kg/m2)
3.1
 
274
829
Weights
Empty weight (kg)
8
 
16,034.5
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
27,759.9
575,000
Loaded weight (kg)
5
 
21,269
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
726
28,165
Сruise Speed (km/h)
52
 
640
3,087
Fuel
Fuel Capacity (l)
23
 
9,961
320,000
Power
Total Power (hp)
0.4
 
10,070
60,000
2 powerplants 5035 hp each
Performance
Service ceiling (m)
0.6
 
11,430
161,544
Range (Ferry range) (km)
4
 
3,508
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
2,078.7
36,000
Combat
Guns (qt)
1
 
2
18
20 mm cannons in tail (never fitted)
Bombs weight (kg)
2
 
4,763
39,000
Stat
Introduction 1952
First flight 04.01.1952

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