McDonnell Douglas F-4 Phantom II Performance, Dimensions, General, Weights, Manufacturer, Model, Country. 25 properties. Comparisons. Similar objects.

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Object «McDonnell Douglas F-4 Phantom II» was created due to

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Object «McDonnell Douglas F-4 Phantom II» has attributes [Show empty attributes][Hide empty attributes]

Attribute	Value
General
Manufacturer	McDonnell Douglas
Model	McDonnell Douglas F-4 Phantom II
Country	United States
Manufactured from	1958 year
Manufactured to	1981 year
Type	Fighter Jets
Icao	F4
Performance
Engine	2x 2 × General Electric J79-GE-17A Turbojets
Power, hp	Add
Power, lbf	17,900 lbf
Avionics	Add
Max cruise speed	2,371 km/h
Approach speed	Add
Travel range	2,815 km
Fuel economy	0.205 km/l
Service ceiling	18,898 m
Rate of climb	209.8 m/sec
Take off distance	1,370 m
Landing distance	1,120 m
Weights
Max take off weight	28,030 kg
Max landing weight	16,706 kg
Max payload	8,500 kg
Fuel tank capacity	12,624 l
Baggage volume	Add
Dimensions
Seats	2
Seats - business class	Add
Seats - first class	Add
Cabin height	Add
Cabin width	Add
Cabin length	Add
Exterior length	19.2 m
Tail height	5 m
Fuselage diameter	Add
Wing span	11.7 m
Wing tips	No Winglets

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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (40 fields were changed)

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