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SW-Version alpha 0.41
Darstellung: System
Sprache: DE

Platform Variants

1. Platform Variants

The F-35 is produced in three variants based on a common basic design, yet differing considerably in their construction. Contrary to frequent claims, the actual commonality between the variants amounts to only around 20% shared structural components [2].

F-35A (CTOL – Conventional Takeoff and Landing)

The F-35A is the primary variant of the US Air Force and the export model for international partners, including Switzerland. It is designed for conventional takeoff and landing on paved runways.

Parameter Value
Top speed Mach 1.6
Combat radius >1,093 km (590 nm)
Service ceiling >15,240 m (50,000 ft)
G-limit +9.0/-3.0 g
Internal fuel capacity 8,278 kg (18,250 lbs)
Empty weight approx. 13,290 kg

Source: USAF Fact Sheet F-35A [3], Lockheed Martin F-35 Brochure [4]

F-35B (STOVL – Short Takeoff and Vertical Landing)

The F-35B is the variant used by the US Marine Corps and the Royal Air Force. It features the Rolls-Royce LiftFan system and a swiveling nozzle that enable short takeoff and vertical landing.

Parameter Value
Combat radius >833 km (450 nm)
Vertical thrust >18,000 kg (combined)
G-limit +7.0 g
Distinguishing feature Smaller weapon bays than F-35A/C

F-35C (CV – Carrier Variant)

The F-35C is the US Navy's carrier variant with a reinforced airframe, tailhook, and folding wings for aircraft carrier operations.

Parameter Value
Combat radius >1,111 km (600 nm)
Wingspan 13.1 m (43 ft) – larger than A/B
G-limit +7.5 g
Distinguishing feature Reinforced landing gear structure, larger wing area

Production Numbers

As of late 2024, over 1,000 F-35s have been delivered to international operators. The annual production rate is approximately 150 aircraft, with a target of 156 per year [5].


References

[2] F35.com: The ABCs of F-35
[3] United States Air Force: F-35A Lightning II Fact Sheet
[4] Lockheed Martin: F-35 Lightning II Brochure (PDF)
[5] GAO-25-107632: F-35 JSF: Actions Needed to Address Late Deliveries. 2025