Search filter

    • Year
      1906
      2018
    • Length
      6 m
      10 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      20 m2
      32 m2
    • Wingspan (Beam)
      11 m
      17 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
      8 kg
      276800 kg
    • Max. takeoff weight (Gross weight)
      2576 kg
      3864 kg
    • Loaded weight
      2848 kg
      4272 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
      360 km/h
      540 km/h
    • Сruise Speed
      291 km/h
      437 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
      768 hp
      1152 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7440 m
      11160 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1028 km
      1542 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
      681 m/min
      1023 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
      34 qt
      52 qt
    • Price
      41 USD
      750000000 USD

Bellanca 28-90 Flash

TypeAircraft
Company

AviaBellanca Aircraft Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.1
88.7
Height (m)
0.6
 
2.6
50.1
Wings
Wing area (m2)
1.1
 
25.9
925
Wingspan (Beam) (m)
0.1
 
14.1
95
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
3,220
575,000
Loaded weight (kg)
5
 
3,560
242,500
Capacity
Crew (per.)
1
 
2
112
pilot and observer
Speeds
Max. Speed (km/h)
25
 
450
28,165
Сruise Speed (km/h)
52
 
364
3,087
Power
Total Power (hp)
0.4
 
960
60,000
Performance
Service ceiling (m)
0.6
 
9,300
161,544
Range (Ferry range) (km)
4
 
1,285
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
852
36,000
Stat
Number built (qt)
0
 
43
43,000
Introduction 1934
First flight 1937

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