WeaponSpecs
Fighter aircraft United States flagUnited States Legacy

Boeing

F-4E Phantom II

Twin-engine, two-seat supersonic interceptor and fighter-bomber originally built by McDonnell Douglas (now Boeing) that served as a mainstay of Cold War-era air forces. The E model added an internal cannon and remains in limited service with a handful of upgraded operators.

In service since 1967 · 5 operator countries

Compiled from public sources ·primary reference ↗ ·last verified 2026-07-02

2,370

km/h

2,600

km range

18,300

m ceiling

8,480

kg payload

0.86

T/W

Pricing: Out of production; historical program cost only

Procurement snapshot

Availability & export

US ITAR-controlled

Export needs U.S. State Dept (DDTC) approval; end-use & re-transfer restrictions apply.

Channel: Foreign Military Sales (FMS) or Direct Commercial Sale

Fielded & proven

Established · 5 operators

In service since 1967. Status: legacy · ~5,195 built.

Lifecycle cost (est.)

No public unit price to model from.

Interoperability

AIM-9 Sidewinder

Derived guidance from public data — export regime by country of origin, lifecycle from the GAO ~30% acquisition rule. Verify eligibility, pricing and offsets with the manufacturer and your acquisition authority.

Full specifications

Performance

Speed, range, altitude and engagement capability.

Max speed

Maximum level speed. For aircraft this is at optimal altitude; for ground vehicles, top road speed. Higher means faster response and better kinematic performance.

2,370 km/h
Stronger than 73% of fighters
Max speed (Mach)

Maximum speed as a multiple of the speed of sound. Mach 2+ is typical for air-superiority fighters.

2.2 Mach
Stronger than 71% of fighters
Range

Maximum distance: ferry range for aircraft, operational range for vehicles, maximum engagement distance for missiles. Higher means more standoff or persistence.

2,600 km
Stronger than 32% of fighters
Combat radius

Distance an aircraft can fly, complete its mission and return without refueling. Roughly a third of ferry range.

680 km
Stronger than 20% of fighters
Service ceiling

Maximum operating altitude. Higher gives energy advantage and sensor horizon.

18,300 m
Stronger than 81% of fighters
Thrust-to-weight

Engine thrust divided by loaded weight. Above 1.0 the aircraft can accelerate going straight up.

0.86
Bottom 8% of fighters

Firepower

Armament, payload and guidance.

Main armament

Primary weapon: main gun, cannon or missile type.

20 mm M61A1 Vulcan rotary cannon
Hardpoints

External stations for weapons and pods. More means bigger and more flexible loadouts.

9
Stronger than 47% of fighters
Weapons payload

Maximum ordnance weight the platform can carry. Higher means more strike capacity per sortie.

8,480 kg
Stronger than 78% of fighters

Protection

Armor, countermeasures and survivability.

Countermeasures

Self-protection: chaff, flares, DIRCM, towed decoys, smoke dischargers, jammers.

chaff, flares

Physical

Dimensions, weight and crew.

Length

Overall length including gun/probe where applicable.

19.2 m
Wingspan

Wingtip-to-wingtip span.

11.7 m
Height

Overall height. Lower profile is harder to spot and hit for ground vehicles.

5.02 m
Empty weight

Weight without fuel, ammunition or crew.

13,800 kg
Combat weight

Fully loaded weight. Lighter eases transport and bridging limits; heavier often means more armor.

20,800 kg
Crew

Personnel required to operate. Fewer reduces exposure; autoloaders trade a loader for mechanical complexity.

2

Propulsion

Engine, power and fuel.

Engine

Powerplant model and type.

2x General Electric J79-GE-17A afterburning turbojets
Engines

Number of engines. Twin-engine gives redundancy at higher cost.

2
Thrust

Total engine thrust (with afterburner where applicable).

79 kN
Stronger than 20% of fighters
Fuel capacity

Internal fuel volume.

7,500 L
Propulsion type

Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet…

Turbojet

Sensors & avionics

Radar, sensor suite and datalinks.

Radar

Primary radar. AESA (active electronically scanned array) is the current state of the art.

AN/APQ-120 (upgraded to AN/APG-65 or similar on modernized aircraft)

Program

Cost, production scale and operators.

Units built

Total production run. Higher means proven manufacturing, mature logistics and spares availability.

5,195
Top 1% of fighters
Operator countries

Number of countries operating the system. More operators means broader support ecosystem.

5
Stronger than 75% of fighters

Specifications compiled from public Boeing and reference sources ↗. Published defense figures are approximations — treat comparisons as directional. Last verified 2026-07-02.

Compare with rivals

See how it stacks up

Frequently asked questions

What is the top speed of the Boeing F-4E Phantom II? +

The Boeing F-4E Phantom II has a maximum speed of 2,370 km/h.

What is the range of the Boeing F-4E Phantom II? +

The Boeing F-4E Phantom II has a maximum range of 2,600 km.

What is the weapons payload of the Boeing F-4E Phantom II? +

The Boeing F-4E Phantom II can carry up to 8,480 kg of weapons payload.

How much does the Boeing F-4E Phantom II weigh? +

The Boeing F-4E Phantom II has a combat weight of 20,800 kg.

How many crew does the Boeing F-4E Phantom II require? +

The Boeing F-4E Phantom II requires a crew of 2.

What is the main armament of the Boeing F-4E Phantom II? +

The Boeing F-4E Phantom II's primary weapon is the 20 mm M61A1 Vulcan rotary cannon.

What engine does the Boeing F-4E Phantom II use? +

The Boeing F-4E Phantom II is powered by the 2x General Electric J79-GE-17A afterburning turbojets.

What is the Boeing F-4E Phantom II used for? +

The Boeing F-4E Phantom II is a fighter aircraft typically used for air superiority, close air support, deep strike.

How many countries operate the Boeing F-4E Phantom II? +

The Boeing F-4E Phantom II is operated by 5 countries.

How much does the Boeing F-4E Phantom II cost? +

Boeing F-4E Phantom II: Out of production; historical program cost only. Defense program costs are rarely fully public and vary by contract and configuration.

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