Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      41 m2
      63 m2
    • Wingspan (Beam)
      17 m
      27 m
    • Wing loading
      280 kg/m2
      420 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
      8306 kg
      12460 kg
    • Max. takeoff weight (Gross weight)
      14345 kg
      21519 kg
    • Loaded weight
      5 kg
      242500 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
      652 km/h
      980 km/h
    • Сruise Speed
      528 km/h
      792 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
      0 hp
      60000 hp
    • Thrust
      28 kN
      44 kN
    • Service ceiling
      9387 m
      14082 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3200 km
      4800 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      1416 km
      2124 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
      602 m/min
      904 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
      8 qt
      12 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2903 kg
      4355 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Douglas B-43 Jetmaster

TypeAircraft
Company

Douglas Aircraft Company

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
15.7
88.7
Height (m)
0.6
 
7.4
50.1
Wings
Wing area (m2)
1.1
 
52.3
925
Wingspan (Beam) (m)
0.1
 
21.7
95
Wing loading (kg/m2)
3.1
 
350
829
Weights
Empty weight (kg)
8
 
10,382.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
17,932
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
816
28,165
Сruise Speed (km/h)
52
 
660
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.2
2.1
Thrust (kN)
1.5
 
36
1,914
2 powerplants 18 kN each
Performance
Service ceiling (m)
0.6
 
11,734.8
161,544
Range (Ferry range) (km)
4
 
4,000
40,700
Сombat radius (km)
277
 
1,770
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
752.9
36,000
Combat
Guns (qt)
1
 
10
18
2 × 0.50 in (12.7 mm) machine guns in a remotely operated tail mount; 8 × 0.50 in (12.7 mm) machine guns in solid nose
Bombs weight (kg)
2
 
3,629
39,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1946
First flight 17.05.1946

Similar aircraft

Get more

Comments