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Tactical Missiles.

AIM-260 JATM.

AIM-260 JATM Joint Advanced Tactical Missile United States specifications technical data review fact sheet pictures video

The AIM-260 Joint Advanced Tactical Missile (JATM) is a U.S. next-generation long-range beyond-visual-range air-to-air missile developed for the U.S. Air Force and U.S. Navy to provide greater engagement reach, improved terminal energy, enhanced resistance to electronic warfare, and advanced network-enabled targeting compared with the AIM-120 AMRAAM.

Country users: Australia, United States

Description

The AIM-260 JATM (Joint Advanced Tactical Missile) is a United States next-generation long-range air-to-air missile developed for the U.S. Air Force and U.S. Navy as a successor to the AIM-120 AMRAAM family. It is designed principally for beyond-visual-range interception of enemy fighters and other high-value airborne targets, with emphasis on longer-range performance and greater ability to defeat electronic-warfare jamming than existing AMRAAM variants. The program is managed within the U.S. military air-to-air weapons enterprise, including the U.S. Navy's Air-to-Air Missiles Program Office PMA-259, which is responsible for acquisition, development, and sustainment of air-to-air missile systems. The manufacturer and many detailed program arrangements remain publicly restricted because of the highly classified nature of JATM.

The AIM-260 became publicly known in 2019 and was developed in response to the increasing reach and sophistication of foreign air-to-air missiles, particularly advanced Chinese weapons. A central design requirement has been to achieve significantly greater range than the AIM-120 while remaining within broadly the same external size envelope, an important consideration for internal carriage aboard low-observable aircraft such as the F-22 Raptor and F-35 Lightning II. Official imagery confirmed by the U.S. Air Force shows a highly streamlined cylindrical airframe with four tail-mounted fins and no visible mid-body aerodynamic surfaces, producing a notably cleaner configuration than the AIM-120. The first public sighting of an actual AIM-260 occurred in May 2026 when the missile was photographed on a U.S. Navy F/A-18F Super Hornet operated by VX-31, confirming that the previously released official renderings closely reflected the physical missile configuration.

The AIM-260 appears to devote a substantial percentage of its internal volume to propulsion. Official imagery and munition markings indicate an elongated solid-rocket motor section compared with the AIM-120, supporting assessments that its increased performance may be obtained partly through more energetic propulsion while retaining a compact external form. Advanced highly loaded propellant technology, a dual-pulse motor arrangement, and thrust-vector control have all been discussed in open-source technical analysis as possible means of improving range, energy retention, and endgame maneuverability; however, none of these specific features has been officially confirmed as part of the operational missile. Its exact dimensions, weight, propulsion architecture, speed, and maximum engagement range remain classified.

The AIM-260 is also expected to introduce a substantially more sophisticated guidance and networked engagement architecture than earlier air-to-air missiles. Its detailed seeker design remains classified, and there is no official public confirmation of an AESA, imaging-infrared, passive RF, or multi-mode seeker arrangement. Advanced network connectivity is nevertheless expected to be central to the weapon's operational concept, allowing targeting information and mid-course updates to be supplied by platforms other than the aircraft that launched the missile. Such an architecture would permit fighters, unmanned aircraft, airborne surveillance platforms, and other distributed sensors to contribute targeting data during long-range engagements. U.S. planning has also linked the AIM-260 with future Collaborative Combat Aircraft, indicating that the weapon is expected to become part of a wider distributed air-combat network rather than functioning solely as a conventional fighter-launched missile.

The AIM-260 program has advanced through flight and live-fire testing toward production and operational fielding. Fiscal Year 2026 U.S. budget documentation included procurement funding associated with the missile, providing a public indication that JATM was moving beyond development and test activities toward acquisition, although the exact production status, inventory size, and operational deployment schedule remain classified. Its international importance increased significantly on 6 August 2026, when the Australian Government announced an investment of almost A$736 million to acquire the AIM-260 for the Royal Australian Air Force. Australia will become the first country outside the United States to operate the missile, with the Australian government describing it as a high-speed, long-range air-to-air weapon. Australian integration is planned first on the F/A-18F Super Hornet, followed by the F-35A Lightning II and EA-18G Growler, establishing the AIM-260 as both a future U.S. long-range air-combat weapon and an emerging allied capability for high-end air warfare in the Indo-Pacific.

AIM-260 JATM variants:

No variants at this time

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Technical Data

  • Design

    The AIM-260 JATM features a slender cylindrical airframe optimized for reduced aerodynamic drag and sustained high-speed flight, with four compact control surfaces concentrated around the rear of the missile and no visible mid-body wings. This arrangement differs substantially from the AIM-120 AMRAAM, which uses four mid-body surfaces together with four rear fins. The cleaner AIM-260 configuration reduces external aerodynamic interference and is consistent with the requirement for improved long-range energy retention. Its precise dimensions remain classified, but the missile was deliberately developed around an AMRAAM-class form factor to facilitate carriage within the restricted internal weapons bays of stealth fighters. The configuration seen in official renderings was physically confirmed in May 2026 when an AIM-260 was publicly photographed on a VX-31 F/A-18F test aircraft.

  • Engine

    The AIM-260 JATM uses solid-rocket propulsion, although the exact motor configuration, propellant composition, impulse characteristics, burn profile, and flight-control architecture remain classified. Official renderings show munition markings consistent with a rocket motor occupying a comparatively large proportion of the missile's total length, suggesting that increased propulsion volume is one factor behind the weapon's extended-range performance. Highly loaded propellant grain technology, dual-pulse propulsion, and thrust-vector control have been proposed in open-source analysis as technically plausible methods of increasing range and preserving maneuvering energy during the terminal phase, particularly given the missile's absence of mid-body aerodynamic surfaces. These features should nevertheless be treated as assessments rather than confirmed AIM-260 specifications.

  • Guidance Systems

    The AIM-260 JATM is designed around an advanced guidance and networked engagement concept, but its precise seeker and datalink configuration remain classified. The missile is expected to receive targeting information and mid-course updates during flight before transitioning to autonomous terminal guidance, enabling engagement of targets at distances beyond the immediate sensor coverage of the launching aircraft. Public analysis has suggested that an advanced active-radar seeker, potentially using electronically scanned-array technology, would provide advantages in target discrimination and resistance to jamming, while multi-mode sensing has also been proposed as a possible capability; neither configuration has been officially confirmed. The broader development of AIM-260 for both crewed fighters and future Collaborative Combat Aircraft indicates strong emphasis on distributed targeting and third-party sensor support across increasingly networked air-combat formations.

  • Warhead

    The AIM-260 JATM is believed to employ a compact high-explosive fragmentation warhead designed to destroy or critically damage airborne targets through a combination of blast pressure and high-velocity fragments, although the exact warhead mass, explosive composition, fragmentation pattern, and fuze architecture remain classified. Official renderings show ordnance markings consistent with an explosive warhead, and the missile's apparent allocation of substantial internal volume to propulsion suggests that the warhead may rely on advanced energetic materials, optimized fragmentation geometry, and a sophisticated proximity fuze to preserve lethality within a relatively compact section of the airframe.

  • Combat Use

    The AIM-260 JATM is intended for long-range beyond-visual-range air combat against advanced fighters and high-value airborne targets such as bombers, airborne early-warning aircraft, tankers, electronic-warfare platforms, and command-and-control aircraft. Its operational concept emphasizes engagement at extended distances, high retained terminal energy, resistance to electronic countermeasures, and network-enabled targeting, allowing the launching aircraft to receive or pass target data through other sensors and potentially prosecute threats beyond its own radar coverage while minimizing exposure to hostile air-to-air weapons.

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Specifications

  • Type

    Next-generation long-range beyond-visual-range air-to-air missile

  • Country users

    Australia, United States

  • Designer Country

    United States

  • Propulsion

    Solid-propellant rocket motor; detailed motor configuration classified

  • Guidance

    Classified; advanced guidance, mid-course updating, network-enabled targeting, and autonomous terminal guidance expected

  • Warhead

    Classified; official imagery displays ordnance markings consistent with an explosive warhead

  • Weight

    ?

  • Speed

    ?

  • Range

    Classified; designed to provide substantially greater long-range performance than the AIM-120 AMRAAM

  • Dimensions

    Classified and not officially disclosed; designed around an approximately AIM-120-compatible dimensional envelope

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