Search filter

    • Year
      1906
      2018
    • Length
      10 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      41 m2
    • Wingspan (Beam)
      11 m
      18 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
      4374 kg
      6562 kg
    • Max. takeoff weight (Gross weight)
      6571 kg
      9857 kg
    • Loaded weight
      5640 kg
      8462 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
      96 km/h
      1500 km/h
    • Max. Speed
      392 km/h
      590 km/h
    • Сruise Speed
      267 km/h
      401 km/h
    • Stall Speed
      108 km/h
      162 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
      899 l
      1350 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
      2240 hp
      3360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1216 km
      1824 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
      841 m/min
      1262 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
      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
      304 qt
      456 qt
    • Price
      41 USD
      750000000 USD

Grumman OV-1 Mohawk

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Midwing

Monoplane

Geometry
Length (m)
1.9
 
12.5
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
33.5
925
Wingspan (Beam) (m)
0.1
 
14.6
95
Weights
Empty weight (kg)
8
 
5,467.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
8,214.1
575,000
SLAR mission
Loaded weight (kg)
5
 
7,051
242,500
Capacity
Crew (per.)
1
 
2
112
pilot, observer
Speeds
Max. Speed (km/h)
25
 
491
28,165
at 3050 m
Сruise Speed (km/h)
52
 
334
3,087
econ cruise
Stall Speed (km/h)
40
 
135
257.7
Fuel
Fuel Capacity (l)
23
 
1,124.3
320,000
Power
Total Power (hp)
0.4
 
2,800
60,000
2 powerplants 1400 hp each
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
1,520
40,700
SLAR mission
Endurance (h)
0.0
 
2
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,051.6
36,000
Stat
Number built (qt)
0
 
380
43,000
Introduction 1959
First flight 14.04.1959
Stop production 01.09.1996

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