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    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      4 m
      7 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 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)
      15943 kg
      23916 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 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
      401 km/h
      603 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      91 km/h
      138 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
      5935 l
      8904 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
      3360 hp
      5040 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7680 m
      11520 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      3485 km
      5228 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
      2 qt
    • Bombs weight
      1280 kg
      1920 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Grumman XTB2F

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Concept

High wing

Monoplane

Geometry
Length (m)
1.9
 
15.9
88.7
Height (m)
0.6
 
5.2
50.1
Weights
Max. takeoff weight (Gross weight) (kg)
154
 
19,929.5
575,000
Capacity
Crew (per.)
1
 
3
112
Speeds
Max. Speed (km/h)
25
 
502.1
28,165
Stall Speed (km/h)
40
 
114.4
257.7
Fuel
Fuel Capacity (l)
23
 
7,419.4
320,000
Power
Total Power (hp)
0.4
 
4,200
60,000
2 powerplants 2100 hp each
Performance
Service ceiling (m)
0.6
 
9,600
161,544
Range PTB (Ferry range) (km)
720
 
4,356.5
10,000
Combat
Torpedoes (qt)
1
 
1
4
Mark 13 torpedo or
Bombs weight (kg)
2
 
1,600
39,000
bombs or mines in bomb bay
Stat
Introduction 1944

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