Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      18 m2
      28 m2
    • Wingspan (Beam)
      9 m
      14 m
    • Wing loading
      280 kg/m2
      420 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
      3375 kg
      5064 kg
    • Max. takeoff weight (Gross weight)
      5969 kg
      8954 kg
    • Loaded weight
      5164 kg
      7748 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      4 qt
      8 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      740 km/h
      1110 km/h
    • Сruise Speed
      619 km/h
      929 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
      1 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      21 kN
      32 kN
    • Service ceiling
      10875 m
      16313 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1680 km
      2520 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
      1253 m/min
      1881 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
      3 qt
      5 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      4 qt
      8 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      1105 qt
      1659 qt
    • Price
      41 USD
      750000000 USD

Grumman XF9F Panther

TypeAircraft
Company

Grumman Aerospace Corporation

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
11.3
88.7
Height (m)
0.6
 
3.8
50.1
Wings
Wing area (m2)
1.1
 
23.2
925
Wingspan (Beam) (m)
0.1
 
11.6
95
Wing loading (kg/m2)
3.1
 
350
829
Weights
Empty weight (kg)
8
 
4,219.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,461.6
575,000
Loaded weight (kg)
5
 
6,456
242,500
Capacity
Crew (per.)
1
 
1
112
Hardpoints (qt)
1
 
6
2,576
Speeds
Max. Speed (km/h)
25
 
925
28,165
Сruise Speed (km/h)
52
 
774
3,087
Power
Thrust/weight (kN/kg)
0.0
 
0.4
2.1
Thrust (kN)
1.5
 
26.5
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
13,594.1
161,544
Range (Ferry range) (km)
4
 
2,100
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,566.7
36,000
Combat
Guns (qt)
1
 
4
18
20 mm (0.79 in) M2 cannon
Rockets (qt)
1
 
6
76
Stat
Number built (qt)
0
 
1,382
43,000
Introduction 1947
First flight 24.11.1947
Stop production 1958

Similar aircraft

Get more

Museums on map

Museums

Comments