Search filter

    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      59 m2
      90 m2
    • Wingspan (Beam)
      18 m
      28 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
      2656 kg
      3986 kg
    • Max. takeoff weight (Gross weight)
      5370 kg
      8056 kg
    • Loaded weight
      4626 kg
      6940 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      1270 kg
      1906 kg
    • Capacity passengers
      12 per.
      18 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      198 km/h
      298 km/h
    • Сruise Speed
      184 km/h
      276 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
      600 hp
      900 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3656 m
      5484 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      991 km
      1487 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
      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
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Fairchild XC-941

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
16.9
88.7
Height (m)
0.6
 
4.8
50.1
Wings
Wing area (m2)
1.1
 
74.5
925
Wingspan (Beam) (m)
0.1
 
22.9
95
Weights
Empty weight (kg)
8
 
3,321
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
6,713
575,000
Loaded weight (kg)
5
 
5,783
242,500
Capacity
Crew (per.)
1
 
1
112
Payload (kg)
23
 
1,587.6
122,470
Capacity passengers (per.)
1
 
15
400
Speeds
Max. Speed (km/h)
25
 
248
28,165
Сruise Speed (km/h)
52
 
230
3,087
Power
Total Power (hp)
0.4
 
750
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,570
161,544
Range (Ferry range) (km)
4
 
1,239
40,700
Stat
Number built (qt)
0
 
1
43,000
Introduction 1934
First flight 22.09.1934

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