Search filter

    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      11 m2
      17 m2
    • Wingspan (Beam)
      6 m
      11 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
      796 kg
      1196 kg
    • Max. takeoff weight (Gross weight)
      1219 kg
      1829 kg
    • Loaded weight
      5 kg
      242500 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
      301 km/h
      453 km/h
    • Сruise Speed
      256 km/h
      384 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
      480 hp
      720 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6681 m
      10022 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      960 km
      1440 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      464 km
      696 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
      175 m/min
      263 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
      3 qt
    • Bombs
      4 qt
      6 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
      120 qt
      182 qt
    • Price
      11207 USD
      16811 USD

Boeing P-26 Peashooter

TypeAircraft
Company

Boeing

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
7.2
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
13.9
925
Wingspan (Beam) (m)
0.1
 
8.5
95
Weights
Empty weight (kg)
8
 
996.1
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,524
575,000
Capacity
Crew (per.)
1
 
1
112
Speeds
Max. Speed (km/h)
25
 
377
28,165
at 1800 m
Сruise Speed (km/h)
52
 
320
3,087
Power
Total Power (hp)
0.4
 
600
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,351.5
161,544
Range (Ferry range) (km)
4
 
1,200
40,700
Сombat radius (km)
277
 
580
7,210
Dynamic Performance
Rate of climb (m/min)
1.9
 
219.2
36,000
Combat
Guns (qt)
1
 
2
18
.30 in (7.62 mm) M1919 Browning machine guns
Bombs (qt)
1
 
2
250
45 kg GP bombs
1
 
5
250
14 kg anti-personnel bombs
Stat
Number built (qt)
0
 
151
43,000
Price (USD)
41.5
 
14,009
750.0 million
Introduction 1932
First flight 20.03.1932
Stop production 1956

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