Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      31 m2
      48 m2
    • Wingspan (Beam)
      12 m
      19 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
      2 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
      4866 kg
      7300 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      7859 kg
      11790 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
      96 km/h
      1500 km/h
    • Max. Speed
      481 km/h
      723 km/h
    • Сruise Speed
      242 km/h
      364 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
      2400 hp
      3600 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6412 m
      9618 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2362 km
      3544 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
      547 m/min
      821 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
      3 m
      6 m
    • Prop blade number
      4 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
      2 qt
    • Bombs weight
      728 kg
      1092 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1 qt
      3 qt
    • Price
      41 USD
      750000000 USD

Curtiss XBTC

TypeAircraft
Company

Curtiss Aeroplane and Motor Company

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.9
88.7
Height (m)
0.6
 
3.9
50.1
Wings
Wing area (m2)
1.1
 
39.5
925
Wingspan (Beam) (m)
0.1
 
15.2
95
Rotors
Rotor number (qt)
1
 
1
8
Weights
Empty weight (kg)
8
 
6,082.7
276,800
Loaded weight (kg)
5
 
9,824.8
242,500
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
601.9
28,165
at 4900 m
Сruise Speed (km/h)
52
 
302.6
3,087
Power
Total Power (hp)
0.4
 
3,000
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,015
161,544
Range (Ferry range) (km)
4
 
2,953
40,700
at 303 km/h
Dynamic Performance
Rate of climb (m/min)
1.9
 
684
36,000
Propellers
Prop diameter (m)
1.8
 
4.3
5.8
Prop blade number (qt)
1
 
6
8
Combat
Guns (qt)
1
 
4
18
20 mm cannon
Torpedoes (qt)
1
 
1
4
Bombs weight (kg)
2
 
910
39,000
Stat
Number built (qt)
0
 
2
43,000
Introduction 1944
First flight 1945

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