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Popeye (missile)
View on WikipediaThe Popeye (Hebrew: פופאי) is a family of air-to-surface missiles developed and in use by Israel, of which several types have been developed for Israeli and export users. A long-range submarine-launched cruise missile variant of the Popeye Turbo has been speculated as being employed in Israel's submarine-based nuclear forces.[1] The United States operated the Popeye under a different designation according to US naming conventions as the AGM-142 Have Nap.
Key Information
Design
[edit]The Popeye is designed for precision attack against large targets from stand off ranges. The standard Popeye and smaller Popeye-Lite are powered by a single-stage solid rocket. Rafael offered a Popeye Turbo air launched variant featuring a jet engine and folding wings for a UK competition specifying a cruise missile with range of at least 320 km (200 mi) in 1994; publicly exposing a lowest possible maximum range for that variant.[2][page needed] An inertial guidance system pilots the missile towards the target; for terminal homing the pilot can control the missile directly via an INS and data link, aiming via either a television or imaging infrared seeker depending on the missile model. It is not necessary for the launching aircraft to direct the missile—control can be passed to another platform while the firing aircraft escapes the area. There are two choices of warhead for the export versions, a 340 kg (750 lb) blast/fragmentation or 360 kg (790 lb) penetrator.
The alleged Israeli submarine-launched cruise missile variant is reported to be jet powered and nuclear armed with a greatly increased range, though according to the Federation of American Scientists "open literature provides little information on this system" but in a May 2000 test launch was tracked for 1,500 km (930 mi).[1]
Air launched variants
[edit]- Popeye (also known as Have Nap)— standard solid-rocket–powered stand off missile, 4.82 m (15 ft 10 in) long and weighing 1,360 kg (3,000 lb) with a 340 kg (750 lb) blast fragmentation or 360 kg (790 lb) I-800 penetrating warhead, inertial and imaging infrared or TV guidance.[3]
- Popeye II or Popeye Lite (also known as Have Lite)— reduced size (shortened to 4.24 m [13 ft 11 in]) and weight version (weight is now 1,125 kg [2,480 lb]) of the Popeye to give light aircraft such as the F-16I Sufa a precision standoff strike capability.[3]
- Popeye Turbo ALCM—The Popeye Turbo air-launched cruise missile, which uses a jet engine and liquid fuel, is approx 6.25 m (20 ft 6 in) long; it is reported to have a range of more than 320 km (200 mi).[4]
- Crystal Maze or Raptor was developed in 2003–2004 to be lighter than Popeye for India, with a range of 100 km (62 mi), weighting 1,100 kg (2,400 lb) and carrying an 80 kg (180 lb) warhead.[5]
- Crystal Maze II or ROCKS is an improved version of Crystal Maze with an enhanced range of 250 km (160 mi). The missile was first test launched in April 2024 from Sukhoi Su-30MKI under Andaman and Nicobar Command. The missile will be mass manufactured in India for Indian Air Force. The missile has the capability to target long range radars and air defence systems in GPS denied environments.[6][7][8]
- Have Rain—A 2004 report indicated that Rafael was developing a new anti-ship version known as the “Have Rain.” The new missile is believed to have a launch weight of 900 kg (2,000 lb), for deployment aboard Lockheed P-3 Orion.[9]
- Spice: In 2000, Rafael promoted a "Smart Precise Impact Cost Effective" (Spice) add-on "smart bomb" guidance kit for Mk 84 bombs, this system was based on the Popeye seekers.[3]
Popeye Turbo Submarine Launched Cruise Missile
[edit]The Popeye Turbo SLCM is a reportedly stretched version of the Popeye Turbo developed for use as a submarine-launched cruise missile (SLCM), which was widely reported—in a US Navy-observed 2002 test in the Indian Ocean—to have hit a target 1,500 km (930 mi) away. It is reasonable to assume that the weapon's range has been extended to the point where it can launch against Tehran and even more Iranian cities from a relatively safe location.[10] It can allegedly carry a 200 kiloton nuclear warhead.[10] It is believed that the stretched Popeye Turbo is the primary strategic second strike nuclear deterrent weapon that can be fired from the 650 mm (26 in) secondary torpedo tubes of the Israeli Dolphin-class submarines.[1] It is believed that the SLCM version of the Popeye was developed by Israel after the US Clinton administration refused an Israeli request in 2000 to purchase Tomahawk long range SLCM because of international MTCR proliferation rules.[11] While the standard Popeye is 533 mm (21.0 in) the Dolphin class submarines have four 650 mm (26 in) torpedo tubes in addition to the six standard 533 mm (21.0 in) tubes allowing for the possibility that a SLCM Popeye derivative may be a larger diameter.[12]
Overview
[edit]The Popeye is compatible with a variety of aircraft from tactical fighters to heavy bombers.[13]
Since their inception, the missiles have gone through a variety of improvement programs designed to increase reliability and reduce costs. These efforts have included changes in the materials and manufacturing processes of the wings, fins and rocket motor, new components in the inertial guidance unit, an upgraded processor, and an improved imaging infrared seeker.
Israel is thought to be using the airframe and avionics to produce a long-range submarine-launched cruise missile with a liquid-fueled jet engine similar to the Popeye Turbo rather than a rocket.[14]
In US use, the Popeye designated as the AGM-142 Have Nap is intended primarily to equip the B-52H, allowing it to attack fixed targets of high value at sufficient range to provide protection from defences. The missile represented the first precision guided munition to be carried by the B-52H.
The London Sunday Times newspaper reported that on 5 July 2013, Israeli Dolphin submarines fired long-range cruise missiles at stores of Russian-made P-800 Oniks anti-ship missiles kept at the Syrian port of Latakia, contradicting an earlier CNN report it had been an air strike.[15] Israel also deploys sub-Harpoon missiles capable of land attack on its Dolphin class submarines.[16]
In the afternoon of 7 December 2014, two formations composed by two Israeli Air Force F-15Is each, fired Popeye missiles against two separate target sites in Syria. Syrian air defense Buk-M2 missile batteries fired two missiles at the incoming attack planes, both were jammed and two Pechora 2M missiles were hastily launched at the four incoming Popeye missiles, shooting one down.[17][unreliable source?]
In the early hours of 30 November 2016, Israeli planes launched air-to-surface Popeye missiles from Lebanese airspace at targets at Sabboura, north-east of Damascus.[18]
In 19 December 2024, the IAF conducted airstrikes against the Houthis in Yemen targeting ports and energy infrastructure at Sanaa. Popeye missiles were carried on F-15s while the newer Rampage missiles were carried on F-16s.[19]
Deployment
[edit]
First developed for use by the Israeli Air Force, it has been in service since 1985.
The United States Air Force first bought a batch of 154 missiles in 1989 followed by a second batch of 54 missiles in 1996.
The Royal Australian Air Force purchased a number of Popeye missiles in the late 1990s for use by the RAAF's F-111 bombers. The F-111 was taken out of Australian service in 2010.[20] It proved difficult to integrate the missiles onto the F-111s and costs were much higher than expected.[21]
Currently, the Turkish Air Force's F-4 2020 Terminator aircraft (which were extensively upgraded by IAI) and the TuAF F-16 CCIP are armed with a Turkish License production version of the Popeye.
Israel and Turkey co-production
[edit]In May 1997, Israel and Turkey signed an agreement valued in excess of US$500 million for the establishment of a joint-venture between Israel's Rafael and Turkey's Turkish Aerospace Industries for the co-production of Popeye I and Popeye II missiles in Turkey.[13]
Operators
[edit]

There have been reports that Israel has exported Popeye and its variants to various countries:[22][23]
Australia: Royal Australian Air Force
India: 30 for Indian Air Force
Israel: Israeli Air Force, Israeli Navy
South Korea: Republic of Korea Air Force (retired in 2024)
Turkey: Turkish Air Force
United States: United States Air Force (retired in 2004)
Specifications
[edit]- Weight : 1,360 kg (3,000 lb)
- Length: 4.82 m (15 ft 10 in)
- Diameter: 533 mm (21.0 in)
- Wingspan: 1.98 m (6 ft 6 in)
- Guidance: Inertial plus imaging infrared or TV
- Engine: Single-stage solid rocket
- Range: 78 km (48 mi)
- Warhead: 340 kg (750 lb) blast fragmentation, or 360 kg (790 lb) I-800 penetrating
See also
[edit]References
[edit]- Citations
- ^ a b c Israeli missile. FAS
- ^ NTI.
- ^ a b c "Cruise". Missile threat. Archived from the original on 2009-10-14. Retrieved 2012-08-25 – via Portuguese Web Archive.
- ^ "Emerging Biocruise Threat". AF. USAF Counterproliferation Center. Archived from the original on March 5, 2001.
- ^ "Popeye". Missile Threat. CSIS. Retrieved 2020-03-19.
- ^ "India successfully tests new 250 km strike range air-launched ballistic missile". India Today. 2024-04-23. Retrieved 2024-04-24.
- ^ "IAF successfully tests air-launched ballistic missile in Andamans, significantly boosts stand-off capabilities". The Economic Times. 2024-04-23. ISSN 0013-0389. Retrieved 2024-04-24.
- ^ "India successfully tests Crystal Maze-2 missile capable of striking targets up to 250 kilometres away". WION. 2024-04-23. Retrieved 2024-04-24.
- ^ Pike, John. "AGM-142 Raptor / Have Nap / Popeye - Smart Weapons". Global security. Retrieved 8 October 2015.
- ^ a b Mizokami, Kyle (6 December 2017). "Israel Has a Submarine That Could Destroy Entire Nations (Armed with Nuclear Weapons)". National interest.
- ^ "Submarine Proliferation - Israel Current Capabilities". Nuclear Threat Initiative. Archived from the original on July 4, 2007. Retrieved July 29, 2017.
- ^ "SSK Dolphin Class Submarine". Naval Technology. Retrieved 8 October 2015.
- ^ a b "AGM-142 Raptor / Have Nap / Popeye - Smart Weapons". Retrieved 8 October 2015.
- ^ John Pike. "Popeye Turbo". Retrieved 8 October 2015.
- ^ Ben Hartman (14 July 2013). "Report: Israeli submarine strike hit Syrian arms depot". The Jerusalem Post. Reuters. Retrieved 23 March 2014.
- ^ John Pike. "AGM-84 Harpoon/SLAM - Smart Weapons". Retrieved 8 October 2015.
- ^ War Is Boring (12 December 2014). "Four Israeli F-15s Dodged Syrian Missile Fire to Attack Urgent Targets — War Is Boring". Medium. Retrieved 8 October 2015.
- ^ "Syria conflict:Israeli jets strike outside Damascus". BBC News. 30 November 2016. Retrieved 1 December 2016.
- ^ Newdick, Thomas (19 December 2024). "Israeli Air Force Strikes Yemen With Popeye And Rampage Standoff Missiles". The War Zone. Retrieved 25 December 2024.
- ^ Dodd, Mark (3 December 2010). "RAAF puts F-111 out to pasture". The Australian. Archived from the original on December 3, 2010.
- ^ La Franchi, Peter (19 May 2000). "Missile costs blow out to $395m". Australian Financial Review. Retrieved 27 April 2024.
- ^ "Israel". NTI. Archived from the original on 9 February 2016. Retrieved 25 August 2012.
- ^ "Popeye-2". Missile threat. Archived from the original on 13 August 2007. Retrieved 25 August 2012.
- Bibliography
- Bonds, Ray and David Miller (2002). Illustrated Directory of Modern American Weapons. Zenith Imprint. ISBN 978-0-7603-1346-6.[permanent dead link]
External links
[edit]Popeye (missile)
View on GrokipediaDevelopment and History
Origins and Initial Development
The Popeye missile was developed by Rafael Advanced Defense Systems, an Israeli state-owned defense contractor, in response to the Israeli Air Force's need for a standoff air-to-surface precision-guided munition capable of engaging high-value targets beyond visual range.[1] Development began in the early 1980s, building on Rafael's prior research into television (TV) guidance systems dating back to 1972, with the initial Popeye-1 variant designed as a medium-range, electro-optically guided cruise missile powered by a solid-propellant rocket motor.[5][1][3] The missile's origins trace to Israel's strategic imperative for enhanced strike capabilities against defended targets, incorporating TV guidance for terminal-phase accuracy and a heavy warhead to ensure penetration of hardened structures, distinguishing it from shorter-range munitions like the AGM-65 Maverick.[4] Initial testing focused on air-launch integration with Israeli combat aircraft such as the F-4 Phantom II and F-16 Fighting Falcon, emphasizing standoff range to minimize exposure to enemy air defenses.[2] Popeye entered operational service with the Israeli Air Force in 1985, marking Rafael's first major production of a family of standoff missiles that would later expand to include turbojet-powered variants.[7] The United States subsequently evaluated and adopted the missile under the designation AGM-142 Have Nap, with initial imports from Israel in the late 1980s for U.S. Air Force testing, reflecting its proven reliability in Israeli operational doctrine.[6][3]Evolution of Variants
The Popeye missile entered Israeli Air Force service in 1986 as an air-launched, solid-propellant rocket-powered standoff weapon with television or imaging infrared guidance, enabling precision strikes at ranges of approximately 80 kilometers against high-value targets.[1] Developed by Rafael Advanced Defense Systems from electro-optical guidance research dating to 1972, the original Popeye 1 weighed 1,360 kilograms and carried a 350-kilogram warhead, prioritizing accuracy with a circular error probable of 3 meters.[1] A lighter derivative, the Popeye 2 (also known as Have Lite), followed with testing in 1994 and operational deployment in 1995; at 1,135 kilograms, it incorporated GPS-augmented inertial navigation for improved autonomy over 75 kilometers, facilitating integration on fighter aircraft with payload constraints.[1] The United States integrated the Popeye into its arsenal as the AGM-142 Have Nap from 1988 onward, evolving from late-1980s Pyramid glide bomb technology, with production starting in 1989 and combat readiness by 1992; key sub-variants included the AGM-142A with television seeker and blast-fragmentation warhead, the AGM-142B with imaging infrared seeker, and later AGM-142C/D models featuring 350-kilogram penetrator warheads for hardened targets, alongside export adaptations like the AGM-142E for Australian F-111C aircraft.[3] Producibility enhancements under programs like PEP III, tested in 1998, refined reliability and seeker options such as Z-band or CCD imaging.[3] To achieve extended standoff ranges, Rafael introduced the Popeye Turbo variant post-1994, substituting rocket propulsion with a turbofan engine and folding wings for cruise flight exceeding 200 kilometers in air-launched mode, attaining initial fielding with the Israeli Defense Forces in 2002 following submarine test launches in May 2000.[1][8] The submarine-launched Popeye Turbo configuration, deployable from Dolphin-class vessels, reportedly extends to 1,500 kilometers and supports a 200-kilogram warhead potentially configured for nuclear delivery, marking a shift toward strategic deterrence capabilities.[8][4]Export and Co-Production Efforts
The primary co-production effort for the Popeye missile involved Turkey, initiated through a bilateral defense agreement signed on May 18, 1997, valued at approximately $100 million for the joint production of the Popeye II variant.[9] This partnership established a joint venture between Israel's Rafael Advanced Defense Systems and Turkey's Turkish Aerospace Industries (TAI), enabling local assembly and manufacturing of Popeye I and II missiles.[1] Under the deal, Turkey initially ordered 30 missiles, with the first 20 delivered directly by Rafael, while subsequent production exceeding 170 units occurred domestically through licensed manufacturing and assembly by Turkish firms Roketsan and Mikes.[10][1] Export sales complemented these co-production initiatives, with Rafael securing contracts for Popeye variants to Australia, India, and South Korea.[11] Australia acquired the AGM-142E export variant, adapted for integration with Royal Australian Air Force F-111 aircraft, incorporating performance enhancement packages for standoff operations.[3] India received approximately 30 Popeye missiles for use by the Indian Air Force, primarily on Mirage 2000 fighters, as part of broader Israel-India defense cooperation.[1] South Korea integrated Popeye systems into Republic of Korea Air Force platforms, enhancing long-range precision strike capabilities.[11] These efforts reflected Israel's strategy to leverage the Popeye's modular design for international markets, though specific quantities and timelines for non-Turkish exports remain limited in public disclosures due to classification.[1] The U.S. designation as AGM-142 (Have Nap/Raptor) facilitated allied interoperability but involved licensed production rather than direct export sales.[3] By the early 2000s, some operators like Australia considered divesting stockpiles to fund newer systems, indicating evolving procurement priorities.[12]Technical Design
Air-Launched Configurations
The air-launched Popeye missile, developed by Rafael Advanced Defense Systems in the early 1980s, serves as a standoff air-to-surface weapon primarily employing turbojet propulsion in its baseline configuration, with a solid-fuel rocket booster for initial launch.[1] The standard variant, designated AGM-142A Have Nap in U.S. service, measures approximately 5 meters in length and weighs 1,360 kg at launch, featuring television-guided terminal homing for precision strikes against fixed targets. This configuration was integrated on Israeli F-15 Eagle fighters for extended-range engagements, enabling launches from beyond enemy air defenses.[13] A lighter derivative, the Popeye II (also known as Popeye Lite or AGM-142B Have Lite), optimized for multirole fighters, reduces weight to around 750 kg while maintaining a 150 km range, with electro-optical guidance for improved accuracy in contested environments.[6] Introduced into Israeli service around 1995 following F-16 drop tests in 1994, it prioritizes compatibility with smaller aircraft pylons, such as those on the F-16 Fighting Falcon, allowing for two-missile loads per sortie.[1] Export integrations include Turkish F-4 Phantom II aircraft, which conducted operational firings, and South Korean F-4s, which performed final live tests of AGM-142 Popeye missiles on April 18, 2024, prior to Phantom retirement.[14] The AGM-142E Raptor variant, adapted for U.S. and Australian use, incorporates modifications like GPS-aided navigation for all-weather capability and was certified for carriage on platforms including the U.S. B-52H Stratofortress and Australian F-111C/G strike aircraft, with ranges extended to approximately 120-150 km depending on launch altitude.[15] These configurations emphasize subsonic flight profiles post-boost, with warheads typically ranging from 350 to 400 kg of high explosive, though nuclear-capable options have been associated with Israeli variants in unconfirmed reports from defense analyses.[16] A proposed Popeye Turbo air-launched cruise missile (ALCM) variant, featuring a turbofan engine and folding wings for 200-350 km range, was offered for export competitions but saw limited adoption compared to submarine-focused iterations.[16]Submarine-Launched Popeye Turbo
The submarine-launched Popeye Turbo (SLPT), also known as the Popeye Turbo SLCM, is a variant of the Israeli-developed Popeye Turbo cruise missile adapted for underwater launch, primarily to equip Dolphin-class submarines with a sea-based second-strike capability. Developed by Rafael Advanced Defense Systems after 1994, the SLPT evolved from the air-launched Popeye Turbo, which entered service in 2002, with a reported test of the submarine version conducted in May 2000 in the Indian Ocean.[1][8] This variant utilizes turbofan propulsion and is launched from enlarged 650 mm torpedo tubes on the submarines, enabling deployment from platforms like the INS Dolphin, Leviathan, and later Dolphin II-class vessels such as INS Tanin and Rahav.[17] Specifications for the SLPT remain classified, but estimates indicate a length exceeding 4.82 meters, a diameter compatible with 650 mm tubes, and a range of approximately 1,500 km, as reported from the 2000 test and aligned with requirements for reaching distant targets like Iran from patrol areas.[1][8] However, U.S. intelligence assessments, such as those from the National Air and Space Intelligence Center in 2013, place the Popeye Turbo's range at over 300 km, raising questions about its sufficiency for a credible nuclear deterrent against far-off threats without forward basing.[4] Guidance systems mirror the air-launched model, incorporating inertial navigation, television or imaging infrared seekers, and optional man-in-the-loop control for terminal precision.[1] The missile is believed capable of carrying a nuclear warhead, potentially a 200 kg device with a yield derived from 6 kg of plutonium, though Israel maintains ambiguity regarding its nuclear arsenal and delivery systems.[8] Deployment of the SLPT enhances Israel's strategic posture by providing survivable, mobile nuclear forces independent of land-based assets, with five Dolphin-class submarines operational as of 2016 and a sixth, INS Drakon, anticipated to feature vertical launch systems for improved missile capacity.[17] No exports or operational uses have been confirmed, and details are speculative due to Israel's policy of neither confirming nor denying such capabilities, though analysts widely associate the system with the submarines' role in nuclear deterrence.[4][1]Guidance, Propulsion, and Payload Options
The Popeye missile utilizes an inertial navigation system (INS) augmented by GPS for mid-course guidance, achieving stable flight en route to the target area. Terminal guidance employs electro-optical seekers, selectable between television (TV) for clear-weather operations or imaging infrared (IIR) for all-weather capability, with reported circular error probable (CEP) accuracies of 3 meters or better. A two-way data link enables real-time updates and man-in-the-loop control from the launch platform, allowing mid-flight target redesignation or abort commands.[1][13][6] The Popeye Turbo variant retains similar guidance architecture but incorporates enhancements for submarine launch, including a pop-up trajectory from underwater to achieve low-altitude cruise, followed by INS/GPS mid-course and electro-optical terminal phases. These systems ensure precision against hardened or mobile targets, with the data link facilitating integration with command-and-control networks.[8][2] Propulsion for the standard air-launched Popeye relies on a turbojet engine for sustained subsonic cruise following an initial boost phase, supporting ranges of 80-90 km at speeds around Mach 0.8. The Popeye Turbo employs an advanced liquid-fueled turbojet for extended endurance, enabling ranges of 200-350 km while maintaining low-altitude flight profiles to evade detection. This turbofan-like efficiency distinguishes it from rocket-only systems, allowing loitering or variable-speed operations in some configurations.[18][2][8] Payload options include modular warheads of approximately 350 kg, with conventional blast-fragmentation types for area effects or penetrator variants (e.g., I-800 series) for bunker-busting, achieving deep penetration against reinforced concrete. Export models offer 340 kg blast-fragmentation or 360 kg penetrator warheads, while the Popeye Turbo is assessed as nuclear-capable with yields up to 200 kilotons, though Israeli policy maintains strategic ambiguity on such armaments. Warhead selection depends on mission requirements, with fuzing options for impact, delay, or proximity detonation.[1][3][2]Specifications and Performance
Physical Characteristics
The Popeye missile, also designated AGM-142 in its U.S. export variant as Have Nap, measures 4.82 meters in length, with a diameter of 0.533 meters and a wingspan of approximately 1.98 meters.[1][19] Its launch weight is 1,360 kilograms, including a warhead typically weighing 340 to 360 kilograms of high explosive or penetrator type.[1][19] The missile's cylindrical fuselage incorporates pop-out wings and control surfaces for stability and maneuverability during flight.[3] The Popeye Turbo variant, adapted for submarine and air launch, features a stretched fuselage to accommodate a turbojet engine, increasing its length beyond the baseline model while expanding the diameter to 0.65 meters.[2] This configuration supports extended range operations, with the added volume housing fuel and propulsion components distinct from the solid-rocket motor of the standard Popeye.[8] A lighter derivative, Popeye Lite or Popeye 2, reduces dimensions to 4.24 meters in length and maintains a 0.53-meter diameter, with a decreased weight suitable for integration on smaller platforms.[7] These physical adaptations reflect the missile's modular design, prioritizing compatibility with Israeli and export aircraft such as the F-4 Phantom and F-15 Eagle.[1]Operational Parameters
The Popeye missile family employs a low-observable design optimized for standoff strikes, with operational ranges determined by variant, launch altitude, and payload configuration. The baseline air-launched Popeye (also designated AGM-142) achieves 75-90 km when released from medium-altitude fighter platforms, with effective standoff exceeding 50 nautical miles from high-altitude releases due to initial kinetic energy and aerodynamic lift.[1][15] These parameters support sea-skimming or terrain-hugging flight profiles at altitudes below 100 meters to evade radar detection, though exact cruise altitudes remain classified and vary with mission requirements.[20] The Popeye Turbo variant, utilizing turbofan propulsion for sustained cruise, extends air-launched range beyond 200 km, while its submarine-launched configuration (SLCM) has demonstrated up to 1,500 km in tests conducted around May 2000, enabling second-strike capabilities from Dolphin-class submarines via 533 mm or 650 mm torpedo tubes.[8][1] Propulsion in the baseline model relies on a single-stage solid rocket for boost-glide operation, limiting endurance to minutes, whereas the Turbo's jet engine supports flight durations of 20-30 minutes at subsonic speeds, prioritizing fuel efficiency over velocity for extended loiter and terminal maneuvers.[8] Launch parameters require carrier aircraft speeds above Mach 0.8 and altitudes from sea level to 12 km, with compatibility across platforms like F-4, F-15, and F-16 fighters; submarine launches demand capsule encapsulation for underwater ejection.[1] Environmental tolerances include operation in adverse weather, with inertial navigation augmented by electro-optical seekers ensuring 3 m CEP accuracy under man-in-the-loop control for dynamic targets.[1]| Variant | Range (km) | Propulsion | Typical Flight Profile |
|---|---|---|---|
| Popeye/AGM-142 | 75-90 | Solid rocket boost-glide | Low-altitude ingress, terminal dive |
| Popeye Turbo (air-launched) | >200 | Turbofan cruise | Terrain-following, subsonic sustain |
| Popeye Turbo SLCM | ~1,500 (tested) | Turbofan cruise | Sea-skimming post-ejection[8][1] |
