France conducts first supersonic launch of MICA NG air-to-air missile from Rafale jet.

France has successfully launched an MICA NG air-to-air missile from a Rafale fighter during supersonic flight, marking a key step in validating the weapon for real-world combat conditions; the June 1, 2026, trial at the DGA missile test range focused on whether the missile’s infrared seeker could maintain performance after exposure to the intense thermal stress generated by high-speed flight. The test matters because future air combat increasingly depends on reliably detecting and engaging low-signature aircraft, cruise missiles, and drones during fast-moving interception missions.

The firing confirmed seeker acquisition, target tracking, missile guidance, and aircraft-weapon integration during a supersonic launch profile, reinforcing confidence in one of the MICA NG’s most important technological advances. Combined with new imaging infrared and AESA radar seekers, a dual-pulse rocket motor, and network-enabled engagement modes, the missile is designed to give Rafale pilots greater reach, survivability, and flexibility against increasingly difficult airborne threats.

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The first supersonic flight test launch of the MICA NG air-to-air missile from a Rafale fighter jet evaluated the structural integrity and tracking capability of the imaging infrared seeker under extreme aerodynamic heating conditions. (Picture source: Dassault Aviation)

On June 1, 2026, France carried out the first launch of an MICA NG missile from a Rafale fighter in supersonic flight, as part of a development program that is now moving toward qualification of specific subsystems under operationally relevant conditions. The firing was conducted at the Mediterranean test range of DGA Essais de missiles with participation from MBDA, Dassault Aviation, and the French Air and Space Force. It followed the first guided MICA NG firing from a Rafale on June 19, 2025, which focused on validating the missile's infrared guidance chain against a target.

Rather than determining whether the missile could separate safely from the fighter, acquire a target, and complete an engagement sequence, the second trial concentrated on the behavior of the infrared seeker after exposure to the thermal stress associated with supersonic carriage and launch. Under the 2019-2025 Military Programming Law, France has ordered 567 operational MICA NG missiles in late 2018 and March 2021, in addition to training rounds, to progressively replace existing MICA inventories across Rafale, Mirage 2000-5, and upgraded Mirage 2000D fleets during the coming decade. 

The choice of the infrared-guided MICA IR NG for the trial is significant because aerodynamic heating directly affects the performance of infrared sensors. During flight above Mach 1, friction between the airflow and the missile structure increases temperatures across the missile body, particularly around the seeker window located at the front of the weapon. For an imaging infrared seeker, target acquisition depends on the thermal contrast between the target and its surrounding background. As ambient temperatures rise, that contrast decreases. A fighter jet, cruise missile, or drone that remains detectable under normal conditions becomes more difficult to distinguish when the sensor itself is exposed to elevated temperatures and the surrounding atmosphere generates additional thermal noise.

This affects detection range, target discrimination, and track stability. The June 2026 firing was therefore intended to determine whether the missile could maintain seeker performance under conditions likely to be encountered during high-speed interceptions. According to the test objectives, the launch validated seeker acquisition, tracking performance, missile guidance, aircraft-missile integration, and overall weapon employment during a supersonic launch profile. The fact that this objective was selected for the second development firing indicates that confidence in the basic flight characteristics of the missile had already been established during earlier testing. 

The seeker itself represents one of the most important changes introduced by the MICA NG. France is developing two versions of the missile that share the same airframe, dimensions, and aerodynamic characteristics. The MICA IR NG uses a passive imaging infrared seeker, while the MICA EM NG uses an active electronically scanned array radar seeker. The common airframe allows both versions to be carried interchangeably on the Rafale while preserving identical handling characteristics and launch procedures. The infrared variant offers a passive engagement mode because it does not emit radar energy during terminal homing.

The radar-guided version, for its part, provides all-weather capability and engagement flexibility against targets flying above or below the launch aircraft. The infrared seeker now uses a matrix imaging sensor rather than the seeker architecture employed by earlier MICA variants. Increased onboard processing power is intended to improve detection and classification of low-signature targets, particularly cruise missiles, unmanned aerial vehicles, and aircraft designed to reduce their infrared signature. The radar-guided version introduces an AESA seeker, replacing the previous radar seeker architecture used by the MICA (Missile d'Interception, de Combat et d'Auto-défense).

Both variants are intended to address a threat environment in which reduced radar cross-sections and lower thermal signatures are becoming increasingly common. While the external appearance of the missile remains largely unchanged, the internal architecture has undergone an extensive redesign. The MICA NG retains the dimensions of the current MICA missile: 3.1 m in length, 160 mm in diameter, and a weight of 112 kg. Internally, however, propulsion, electronics, sensors, and computing architecture have all been replaced. Miniaturization of electronic components created additional internal volume that was subsequently allocated to propulsion and seeker improvements.

The MICA NG also retains the over-the-shoulder engagement capability already demonstrated by earlier MICA variants, allowing the missile to engage a target located behind the launching aircraft after target designation and post-launch acquisition. The guidance architecture combines inertial navigation, a two-way datalink, and terminal seeker guidance, while the datalink enables target updates after launch and allows the missile to receive revised target information in flight. This is particularly relevant when engaging maneuvering aircraft or targets detected by sensors other than the launching fighter, as the missile also retains both Lock-On-Before-Launch (LOBL) and Lock-On-After-Launch (LOAL) modes.

The latter enables the engagement of targets located outside the seeker's field of view at the moment of launch and allows the MICA NG to exploit targeting information generated elsewhere within a networked force structure. The most consequential change from a kinematic perspective is the introduction of a dual-pulse solid-fuel rocket motor. Earlier MICA variants relied on a conventional solid-fuel motor that delivered most of its energy shortly after launch. Although effective at shorter ranges, that approach inevitably results in declining energy during the latter stages of flight. The MICA NG addresses this limitation through a propulsion system composed of two separate phases.

The first pulse accelerates the missile immediately after launch, while the second pulse can be activated later in the engagement, typically during the terminal phase, to preserve the missile's speed and maneuverability at greater distances from the launch aircraft. The resulting increase in energy retention directly affects the missile's ability to pursue maneuvering targets late in the engagement. MBDA indicates a range increase of up to 40% compared with current MICA variants, meaning that the engagement distance could be estimated at up to 150 km. Maintaining higher terminal energy is also particularly important against fighters executing defensive maneuvers, cruise missiles flying unpredictable trajectories, and targets attempting to defeat the missile through kinematic exhaustion.

Moreover, the missile continues to employ thrust-vector control, ensuring high maneuverability immediately after launch, while long-chord control surfaces support sustained maneuver performance throughout the flight profile. The MICA NG is not intended to replace Meteor missiles within the Rafale arsenal. Instead, the two missiles occupy different segments of the French air-to-air engagement spectrum. The Meteor remains the principal long-range weapon used by the Rafale for beyond-visual-range combat, while the MICA NG covers the short-to-medium-range segment while retaining substantial beyond-visual-range capability.

This approach reflects a long-standing French preference for retaining a missile family capable of covering both close-combat and medium-range interception requirements rather than separating those functions into two completely distinct weapons. The incoming Rafale F4s are expected to carry larger air-to-air missile loads than earlier standards, increasing the value of combining Meteor and MICA NG missiles within a single loadout. The MICA NG's thrust-vector control, high off-boresight capability, helmet-mounted sight integration, and Lock-On-After-Launch functionality also improve engagements at large angles away from the aircraft nose.

MBDA attributes the MICAN NG's 360-degree launch envelope to a combination of off-boresight target designation, post-launch acquisition, and seeker performance. In practical terms, this allows engagements against threats approaching from sectors that would traditionally require aircraft maneuvering before missile launch. Development of the MICA NG officially entered the realization phase in late 2018 with an initial order for 200 missiles, and a second procurement contract signed in 2021 increased the total to 567 operational missiles.

Industrial responsibilities are divided among MBDA, Safran, Thales, and Roxel. Production infrastructure is already being established while additional firings are scheduled across a range of speeds, altitudes, and engagement geometries. The missile is also intended to serve as the basis for future VL MICA NG surface-to-air systems, preserving commonality between air-launched and ground-based applications. From a capability perspective, the emphasis placed on a supersonic infrared-seeker trial is notable because it focuses on the component most affected by aerodynamic heating and one of the subsystems most relevant to future engagements against low-signature targets.

Written by Jérôme Brahy

Jérôme Brahy is a defense analyst and documentalist at Army Recognition. He specializes in naval modernization, aviation, drones, armored vehicles, and artillery, with a focus on strategic developments in the United States, China, Ukraine, Russia, Türkiye, and Belgium. His analyses go beyond the facts, providing context, identifying key actors, and explaining why defense news matters on a global scale.