Search filter

    • Year
      1906
      2018
    • Length
      19 m
      30 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      138 m2
      208 m2
    • Wingspan (Beam)
      32 m
      49 m
    • Wing loading
      132 kg/m2
      198 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
      12907 kg
      19361 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      22928 kg
      34392 kg
    • Crew
      8 per.
      12 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
      264 km/h
      396 km/h
    • Сruise Speed
      184 km/h
      276 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
      3584 hp
      5376 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4800 m
      7200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      5538 km
      8308 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      1 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
      1 m/min
      36000 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      7 min
      11 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
      4 qt
      6 qt
    • Price
      41 USD
      750000000 USD

Breguet 730

TypeAircraft
Company

Breguet Aviation

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
24.4
88.7
Height (m)
0.6
 
8.6
50.1
Wings
Wing area (m2)
1.1
 
173.1
925
Wingspan (Beam) (m)
0.1
 
40.4
95
Wing loading (kg/m2)
3.1
 
165
829
Weights
Empty weight (kg)
8
 
16,134
276,800
Loaded weight (kg)
5
 
28,660
242,500
Capacity
Crew (per.)
1
 
10
112
Speeds
Max. Speed (km/h)
25
 
330
28,165
Сruise Speed (km/h)
52
 
230
3,087
Power
Total Power (hp)
0.4
 
4,480
60,000
4 powerplants 1120 hp each
Performance
Service ceiling (m)
0.6
 
6,000
161,544
Range (Ferry range) (km)
4
 
6,923
40,700
Endurance (h)
0.0
 
0.5
150
Dynamic Performance
Time to altitude (min)
0.6
 
9
105
to 3000 m
Stat
Number built (qt)
0
 
5
43,000
Introduction 1938
First flight 04.04.1938
Stop production 1954

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