Search filter

    • Year
      1906
      2018
    • Length
      12 m
      19 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      18 m
      28 m
    • Wing loading
      85 kg/m2
      129 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      6205 kg
      9308 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      3 per.
      5 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
      301 km/h
      453 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
      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
      1280 hp
      1920 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6949 m
      10425 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1592 km
      2390 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
      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
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      824 kg
      1236 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Martin 146

TypeAircraft
Company

Glenn L. Martin Company

Scheme

Monoplane

Midwing

Geometry
Length (m)
1.9
 
15.5
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wingspan (Beam) (m)
0.1
 
22.9
95
Wing loading (kg/m2)
3.1
 
107.2
829
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
7,756.4
575,000
Capacity
Crew (per.)
1
 
4
112
Speeds
Max. Speed (km/h)
25
 
377
28,165
Power
Total Power (hp)
0.4
 
1,600
60,000
Performance
Service ceiling (m)
0.6
 
8,686.8
161,544
Range (Ferry range) (km)
4
 
1,991
40,700
Combat
Guns (qt)
1
 
3
18
.30 in (7.62 mm) Browning machine guns
Bombs weight (kg)
2
 
1,030
39,000
Stat
Number built (qt)
0
 
1
43,000
First flight 1935

Similar aircraft

Get more

Comments