Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      50 m2
      76 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      206 kg/m2
      310 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
      9280 kg
      13921 kg
    • Max. takeoff weight (Gross weight)
      14201 kg
      21302 kg
    • Loaded weight
      12977 kg
      19467 kg
    • Crew
      4 per.
      6 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
      478 km/h
      719 km/h
    • Сruise Speed
      328 km/h
      493 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
      3200 hp
      4800 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8485 m
      12729 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2624 km
      3936 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
      270 m/min
      407 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
      4 qt
      8 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      1440 kg
      2160 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

North American Aviation XB-28 Dragon

TypeAircraft
Company

North American Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
17.2
88.7
Height (m)
0.6
 
6.7
50.1
Wings
Wing area (m2)
1.1
 
62.8
925
Wingspan (Beam) (m)
0.1
 
22.1
95
Wing loading (kg/m2)
3.1
 
258.1
829
Weights
Empty weight (kg)
8
 
11,600.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
17,751.3
575,000
Loaded weight (kg)
5
 
16,221.8
242,500
Capacity
Crew (per.)
1
 
5
112
Speeds
Max. Speed (km/h)
25
 
598.7
28,165
st 7600 m
Сruise Speed (km/h)
52
 
410.4
3,087
Power
Total Power (hp)
0.4
 
4,000
60,000
2 powerplants 2000 hp
Performance
Service ceiling (m)
0.6
 
10,607
161,544
Range (Ferry range) (km)
4
 
3,280
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
338.4
36,000
Combat
Guns (qt)
1
 
6
18
.50 caliber (12.7mm) AN/M2 machine guns in remote-sighted turrets
Bombs weight (kg)
2
 
1,800
39,000
maximum (910 normal)
Stat
Number built (qt)
0
 
2
43,000
Introduction 1942
First flight 26.04.1942

Similar aircraft

Get more

Comments