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    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      23 m2
      36 m2
    • Wingspan (Beam)
      12 m
      19 m
    • Wing loading
      3 kg/m2
      829 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
      2 qt
      4 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
      2408 kg
      3612 kg
    • Max. takeoff weight (Gross weight)
      3920 kg
      5880 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 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
      312 km/h
      468 km/h
    • Max. Speed
      392 km/h
      588 km/h
    • Сruise Speed
      320 km/h
      480 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
      1120 hp
      1680 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6800 m
      10200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1080 km
      1620 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
      444 m/min
      666 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      5 min
      9 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      2 qt
      4 qt
    • Guns
      4 qt
      6 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      368 kg
      552 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      184 qt
      276 qt
    • Price
      41 USD
      750000000 USD

Breguet 693

TypeAircraft
Company

Breguet Aviation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
9.7
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
29.2
925
Wingspan (Beam) (m)
0.1
 
15.4
95
Rotors
Rotor number (qt)
1
 
3
8
Weights
Empty weight (kg)
8
 
3,010
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
4,900
575,000
Capacity
Crew (per.)
1
 
2
112
Speeds
Ground Speed (km/h)
96.6
 
390
1,500
Max. Speed (km/h)
25
 
490
28,165
at 5000 m
Сruise Speed (km/h)
52
 
400
3,087
at 4000 m
Power
Total Power (hp)
0.4
 
1,400
60,000
2 powerplants 700 hp each
Performance
Service ceiling (m)
0.6
 
8,500
161,544
Range (Ferry range) (km)
4
 
1,350
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
555
36,000
Time to altitude (min)
0.6
 
7.2
105
to 4000 m
Propellers
Prop blade number (qt)
1
 
3
8
Combat
Guns (qt)
1
 
5
18
1 × fixed, forward-firing 20 mm Hispano-Suiza HS.404 cannon; 2 × fixed, forward-firing 7.5 mm (.295 in) MAC 1934 machine guns; 1 × flexible, rearward-firing 7.5 mm (.295 in) MAC 1934 machine gun in rear cockpit; 1 × fixed, rearward-firing 7.5 mm (.295 in) MAC 1934 machine gun in ventral position
Bombs weight (kg)
2
 
460
39,000
Stat
Number built (qt)
0
 
230
43,000
Introduction 1938
First flight 1938
Stop production 1942

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