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F-22 Raptor vs X-31 EFM Vector

F-22 Raptor vs X-31 EFM Vector at a glance — top speed 2,414 vs 1,448 km/h, max takeoff weight 38,000 vs 7,303 kg, built 195 vs 2 units.

Specifications
F-22 Raptor X-31 EFM Vector
Origin country 🇺🇸 United States 🇩🇪 Germany🇺🇸 United States
Category Combat Aircraft Military Special Mission Aircraft
Manufacturer Lockheed Martin Rockwell-MBB
First flight 7 September 1997 11 October 1990
Year introduced 2003 --
Number produced 195 units 2 units
Average unit price $150 million --
Wing area 78.0 m² 21.0 m²
Wingspan 13.6 m 7.3 m
Height 5.1 m 4.4 m
Length 18.9 m 13.2 m
Maximum speed 2414 km/h 1448 km/h
Operational range 3,220 km -- km
Service ceiling 19,812 m 12,192 m
Max. takeoff weight 38,000 kg 7,303 kg
Empty weight 19,700 kg 5,175 kg
Total thrust 2 x 15,876 kgf 1 x 7,257 kgf
Performance Radar Chart

Detailed Comparison

The F-22 Raptor and X-31 EFM Vector sit at opposite ends of aerospace development: the former is a $150 million operational stealth fighter, while the latter was an unarmed, bi-national testbed built to validate high-angle-of-attack aerodynamics. The X-31 tested extreme post-stall maneuvering in the early 1990s using 3D thrust vectoring. The F-22 integrated a conservative 2D version of that technology, combining it with low observability and supercruise to control beyond-visual-range (BVR) engagements.

Development and Design

The Advanced Tactical Fighter program (1981) birthed the F-22 to counter Soviet advances, prioritizing internal weapons bays and radar-absorbent materials to minimize radar cross-section. Lockheed Martin and Boeing utilized titanium alloys and composites to balance the aircraft's structure. In contrast, the joint US-German X-31 program (Rockwell/MBB) constructed a disposable airframe heavily reliant on off-the-shelf components, including F-16 landing gear. The X-31 utilized three external carbon-epoxy jet deflectors and movable canards to manipulate thrust directly at the exhaust, forcing the aircraft through maneuvers impossible with conventional aerodynamic control surfaces.

Specifications and Performances

The F-22 generates 31,752 kgf of thrust from twin Pratt & Whitney F119-PW-100 turbofans, driving a 38,000 kg MTOW platform to Mach 2+ speeds (2,414 km/h) and enabling sustained supercruise without afterburners. The X-31’s single General Electric F404-GE-400 engine produces 4,808 kgf of thrust for a 7,303 kg MTOW, limiting it to 1,448 km/h. While the X-31 achieved a 218 m/s climb rate to map flight control laws at low speeds and extreme angles of attack, the F-22 traded 3D vectoring paddles for 2D pitch-axis nozzles. This compromise preserved the F-22's stealth profile and thermal management while enabling a 19,812 m service ceiling and 3,000 km range.

Deployment and usage

The X-31 completed 108 flights between two airframes before the program ended in 1995, never seeing combat. Its telemetry directly informed flight control software for later fighters. The F-22 achieved Full Operational Capability in 2007, but production was permanently capped at 195 units in 2009 due to $377 million per-unit lifecycle costs and a doctrine shift toward asymmetric warfare.

The Raptor's combat record is defined by uncontested or semi-contested airspace operations:

  • Forward deployments to Kadena Air Base (2007) and Europe (2014) for regional deterrence.
  • Initial combat during Operation Inherent Resolve (2014), deploying GBU-32 JDAMs and acting as an airborne command node over Syria.
  • Early operational groundings caused by onboard oxygen generating system (OBOGS) failures.

Conclusion

The F-22 dictates tactical combat scenarios. Its AN/APG-77 radar, low-observable shaping, and internal AIM-120 payload allow it to destroy threats long before merging into the within-visual-range arenas the X-31 was built to study. The X-31 held the edge strictly in aerodynamic research, generating the raw telemetry required to mature thrust-vectoring control laws. The X-31 fulfilled its narrow mandate as a disposable testbed, while the F-22 successfully militarized those kinematic theories but remains constrained by low fleet numbers, extreme operating costs, and a closed production line.

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Frequently Asked Questions

Which is faster, the F-22 Raptor or X-31 EFM Vector?
The F-22 Raptor is faster with a maximum speed of 2,414 km/h compared to the X-31 EFM Vector's 1,448 km/h, a difference of 966 km/h.
Which can fly higher, the F-22 Raptor or X-31 EFM Vector?
The F-22 Raptor has a higher service ceiling at 19,812 meters (65,000 ft) compared to the X-31 EFM Vector's 12,192 meters (40,000 ft).
Which is heavier, the F-22 Raptor or X-31 EFM Vector?
The F-22 Raptor has a higher maximum takeoff weight at 38,000 kg compared to the X-31 EFM Vector's 7,303 kg.
Which is larger, the F-22 Raptor or X-31 EFM Vector?
The F-22 Raptor is longer at 18.9 meters compared to the X-31 EFM Vector's 13.2 meters.
Which has been built in greater numbers, the F-22 Raptor or X-31 EFM Vector?
The F-22 Raptor has been produced in greater numbers with 195 units compared to 2 units of the X-31 EFM Vector.