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    • Year
      1906
      2018
    • Length
      7 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      22 m2
      34 m2
    • Wingspan (Beam)
      10 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
      1562 kg
      2344 kg
    • Max. takeoff weight (Gross weight)
      154 kg
      575000 kg
    • Loaded weight
      2048 kg
      3072 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
      354 km/h
      532 km/h
    • Сruise Speed
      276 km/h
      416 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
      560 hp
      840 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6827 m
      10242 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      654 km
      982 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
      469 m/min
      705 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      6 min
      10 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
      64 kg
      96 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      48 qt
      72 qt
    • Price
      41 USD
      750000000 USD

Consolidated P-30

TypeAircraft
Company

Consolidated Aircraft Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
9.1
88.7
Height (m)
0.6
 
2.5
50.1
Wings
Wing area (m2)
1.1
 
27.6
925
Wingspan (Beam) (m)
0.1
 
13.4
95
Weights
Empty weight (kg)
8
 
1,953.2
276,800
Loaded weight (kg)
5
 
2,560
242,500
Capacity
Crew (per.)
1
 
2
112
Speeds
Max. Speed (km/h)
25
 
443
28,165
at 7620 m
Сruise Speed (km/h)
52
 
346
3,087
at 4600 m
Power
Total Power (hp)
0.4
 
700
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,534.4
161,544
Range (Ferry range) (km)
4
 
818
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
587
36,000
Time to altitude (min)
0.6
 
7.8
105
to 4600 m
Combat
Guns (qt)
1
 
3
18
2 x 0.30 in (7.62 mm) machine guns firing through the propeller; 1 x 0.30 in machine gun in the rear cockpit
Bombs weight (kg)
2
 
80
39,000
Stat
Number built (qt)
0
 
60
43,000
Introduction 1932
First flight 1934

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