Search filter

    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      10 m2
      17 m2
    • Wingspan (Beam)
      7 m
      12 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
      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
      326 kg
      490 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      489 kg
      735 kg
    • Crew
      1 per.
      2 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
      167 km/h
      251 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      149 km/h
      225 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
      88 hp
      132 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4876 m
      7316 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      1 h
      3 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
      308 m/min
      462 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
      2 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
      104 qt
      156 qt
    • Price
      41 USD
      750000000 USD

Bristol M.1

TypeAircraft
Company

Bristol Aeroplane Company

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
6.2
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
13.5
925
Wingspan (Beam) (m)
0.1
 
9.4
95
Weights
Empty weight (kg)
8
 
408.2
276,800
Loaded weight (kg)
5
 
612
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Ground Speed (km/h)
96.6
 
209
1,500
Сruise Speed (km/h)
52
 
187
3,087
Power
Total Power (hp)
0.4
 
110
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
6,096
161,544
Endurance (h)
0.0
 
1.8
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
385
36,000
Combat
Guns (qt)
1
 
1
18
fixed-forward .303 in (7.7 mm) Vickers machine gun
Stat
Number built (qt)
0
 
130
43,000
Introduction 1917
First flight 14.07.1916

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