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    • Year
      1906
      2018
    • Length
      15 m
      24 m
    • Height
      4 m
      8 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      50 kg/m2
      76 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
      10000 kg
      15001 kg
    • Max. takeoff weight (Gross weight)
      18528 kg
      27794 kg
    • Loaded weight
      17090 kg
      25636 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
      376 km/h
      566 km/h
    • Сruise Speed
      52 km/h
      3087 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3840 hp
      5760 hp
    • Thrust
      16 kN
      24 kN
    • Service ceiling
      9948 m
      14924 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2229 km
      3345 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1320 km
      1980 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
      707 m/min
      1061 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
      4320 kg
      6480 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      114 qt
      172 qt
    • Price
      41 USD
      750000000 USD

North American Aviation AJ Savage

TypeAircraft
Company

North American Aviation

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
19.2
88.7
Height (m)
0.6
 
6.2
50.1
Wings
Wingspan (Beam) (m)
0.1
 
21.8
95
Wing loading (kg/m2)
3.1
 
63.2
829
Weights
Empty weight (kg)
8
 
12,500.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
23,161
575,000
Loaded weight (kg)
5
 
21,363
242,500
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
471
28,165
Power
Thrust/weight (kN/kg)
0.0
 
0.1
2.1
Total Power (hp)
0.4
 
4,800
60,000
2 powerplants 2400 hp each
Thrust (kN)
1.5
 
20
1,914
1 powerplant 20 kN each
Performance
Service ceiling (m)
0.6
 
12,435.8
161,544
Range (Ferry range) (km)
4
 
2,787
40,700
Сombat radius (km)
277
 
1,650
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
883.9
36,000
Combat
Bombs weight (kg)
2
 
5,400
39,000
of conventional bombs or 1 nuclear bomb
Stat
Number built (qt)
0
 
143
43,000
140, and 3 prototypes
Introduction 1948
First flight 03.07.1948
Stop production 1960

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