Search filter

    • Year
      1906
      2018
    • Length
      35 m
      53 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      9 m
      15 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
      2501 kg
      3752 kg
    • Max. takeoff weight (Gross weight)
      5241 kg
      7863 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
      5 qt
      9 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      361 km/h
      543 km/h
    • Сruise Speed
      52 km/h
      3087 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
      763 l
      1145 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
      1144 hp
      1716 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5852 m
      8778 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      741 km
      1113 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      342 km
      514 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
      1 m/min
      36000 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
      3 qt
      5 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
      288 qt
      432 qt
    • Price
      41 USD
      750000000 USD

North American Aviation OV-10 Bronco

TypeAircraft
Company

North American Aviation

Rockwell International

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
44
88.7
Height (m)
0.6
 
4.6
50.1
Wings
Wing area (m2)
1.1
 
27.0
925
Wingspan (Beam) (m)
0.1
 
12.2
95
Weights
Empty weight (kg)
8
 
3,126.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,551.7
575,000
Capacity
Crew (per.)
1
 
2
112
Hardpoints (qt)
1
 
7
2,576
5 fuselage and 2 underwing
Speeds
Max. Speed (km/h)
25
 
452
28,165
Fuel
Fuel Capacity (l)
23
 
953.9
320,000
Power
Total Power (hp)
0.4
 
1,430
60,000
2 powerplants 715 hp each
Performance
Service ceiling (m)
0.6
 
7,315
161,544
Range (Ferry range) (km)
4
 
927
40,700
Сombat radius (km)
277
 
428
7,210
Combat
Guns (qt)
1
 
4
18
7.62x51mm M60C machine guns
Stat
Number built (qt)
0
 
360
43,000
Introduction 1965
First flight 16.07.1965
Stop production 1995

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