{"id":862,"date":"2026-09-08T11:58:46","date_gmt":"2026-09-08T11:58:46","guid":{"rendered":"https:\/\/poznayu.com\/en\/?p=862"},"modified":"2026-09-08T11:58:46","modified_gmt":"2026-09-08T11:58:46","slug":"storm-shadow-specs-range-and-key-features","status":"publish","type":"post","link":"https:\/\/poznayu.com\/en\/storm-shadow-specs-range-and-key-features\/","title":{"rendered":"Storm Shadow: Specs, Range and Key Features"},"content":{"rendered":"<div style='text-align:right' class='yasr-auto-insert-visitor'><\/div><p class=\"isSelectedEnd\"><span>The experience of military conflicts in the late twentieth century, particularly the 1991 Multinational Force operation in Iraq, demonstrated a critical need for long-range precision weapons for Western air forces.<\/span><\/p>\n<p><!--more--><\/p>\n<p class=\"isSelectedEnd\"><span>Attempts to penetrate dense, layered air defense systems using free-fall bombs or short-range missiles created an unjustifiable risk to manned aircraft and resulted in aircraft losses.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The military needed a weapon capable of reliably destroying strategic, heavily protected targets deep behind enemy lines while allowing launch aircraft to fire from a safe area outside the engagement range of enemy surface-to-air missile systems.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>At the same time, European nations were seeking greater strategic autonomy from U.S. technology solutions such as the Tomahawk and AGM-86 cruise missiles.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The foundation for the future weapon was the French Apache stand-off air-launched missile, designed to disable runways. It already featured the required low-observable aerodynamic shape and terrain-following flight capability. Reworking the concept from dispersing submunitions to delivering a single powerful penetrating warhead against bunkers and command centers became the basis for the new British CASOM (Conventionally Armed Stand-Off Missile) program.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>In the second half of the 1990s, the UK Ministry of Defence formalized its technical and operational requirements, leading to a joint effort with France, which had similar requirements for a strike weapon.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The merger of Britain\u2019s operational requirement for deep-strike capability with France\u2019s technological developments ultimately led to the decision to create a single European platform. The program made it possible to share the enormous financial cost of development, and in the early 2000s the new system officially entered service, receiving its first combat use in the 2003 Iraq War.<\/span><\/p>\n<h2><span>Development<\/span><\/h2>\n<p><img decoding=\"async\" src=\"https:\/\/poznayu.com\/wp-content\/uploads\/2026\/09\/strom-shadow_rocket.jpg\" class=\"aligncenter\" \/><\/p>\n<p class=\"isSelectedEnd\"><span>The missile\u2019s development was the result of large-scale consolidation across the European aerospace industry.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Initial design work was conducted by the Matra BAe Dynamics consortium, which later evolved into the major pan-European missile company MBDA. Combining British and French engineering resources brought together leading expertise in low-observable shaping, advanced composite materials, and autonomous navigation systems. The joint venture also took responsibility for integrating cross-border supply chains, enabling serial production of a highly sophisticated aerodynamic weapons system.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Engineers faced an exceptionally difficult technical challenge: combining stealth, autonomous low-altitude flight, and devastating penetration capability in a compact 1,300-kilogram body.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>To achieve these goals, designers selected the compact Microturbo TRI 60-30 turbojet, providing a stable cruise speed of about Mach 0.8. The engineers rejected a conventional cylindrical fuselage in favor of a faceted profile approximately 630 mm wide and 480 mm high, with folding wings, drastically reducing radar visibility. The weapon\u2019s employment architecture was built around a \u201cfire-and-forget\u201d principle \u2014 the missile flies fully autonomously using a mission profile loaded on the ground, with no need for communication with the launch aircraft after firing.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Development of the system did not stop with the early-2000s baseline version, as the weapon required regular adaptation to modern electronic warfare conditions.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>In the UK, a major Mid-Life Refurbishment (MLR) program was launched, also known as SPEAR Capability 4, including engine life extension work and a major navigation-system upgrade to protect against deliberate GPS jamming. The upgraded missiles began entering service in early 2022. As of 2026, according to the OCCAR agency\u2019s business plan, the program remains active: the UK and France have entered new classified agreements to procure additional batches while simultaneously developing a successor to the system.<\/span><\/p>\n<h2>Pros and Cons<\/h2>\n<p><img decoding=\"async\" src=\"https:\/\/poznayu.com\/wp-content\/uploads\/2026\/09\/strom-shadow_rocket-2.jpg\" class=\"aligncenter\" \/><\/p>\n<p>&nbsp;<\/p>\n<ul data-spread=\"false\">\n<li><span>The primary advantage of the Storm Shadow system is its exceptional survivability when penetrating modern integrated air defense systems.<\/span><\/li>\n<\/ul>\n<p class=\"isSelectedEnd\"><span>This is achieved through a combination of a low-observable airframe (reduced radar cross-section) and an extremely low-altitude terrain-hugging flight profile. A multilayer autonomous navigation system allows the missile to reach its target accurately even under heavy electronic interference, when satellite navigation signals are completely distorted or unavailable.<\/span><\/p>\n<ul data-spread=\"false\">\n<li><span>A second key advantage is the unique BROACH (Bomb Royal Ordnance Augmenting Charge) tandem blast\/penetrator warhead.<\/span><\/li>\n<\/ul>\n<p class=\"isSelectedEnd\"><span>Unlike standard aerial bombs, this 450-kilogram warhead operates sequentially: first, a shaped-charge penetrator cuts a deep channel through the barrier, after which the main warhead enters the opening and detonates with a programmed delay. Official data confirms that the warhead can penetrate more than one meter of reinforced concrete, enabling the destruction of buried bunkers, hardened aircraft shelters, and command posts.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Despite its outstanding effectiveness, the system has clear tactical limitations, primarily its lack of flexibility after launch:<\/span><\/p>\n<ol data-spread=\"false\" start=\"1\">\n<li><span>In the original architecture, in-flight retargeting is publicly described as unavailable; the route and target are determined during ground mission planning. This makes the weapon ineffective against mobile targets or objects whose coordinates have changed rapidly.<\/span><\/li>\n<li><span>In addition, the highly complex electronics, imaging infrared seeker, and radar-signature reduction technologies make each missile extremely expensive, ruling out large-scale use against routine tactical targets.<\/span><\/li>\n<\/ol>\n<p class=\"isSelectedEnd\"><span>Another vulnerability factor is its subsonic flight speed, reaching about 1,000 km\/h (Mach 0.8) during the cruise phase, with possible short-term acceleration to 1,150\u20131,160 km\/h (Mach 0.95), according to current open-source references.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>If the adversary manages to detect the missile, for example using airborne early warning and control aircraft, the subsonic target becomes vulnerable to interception by modern short- and medium-range surface-to-air missile systems because it lacks the kinetic speed needed to evade defensive fire during the terminal phase.<\/span><\/p>\n<div contenteditable=\"false\">\n<hr \/>\n<\/div>\n<p class=\"isSelectedEnd\"><span>Russia, for example, cannot guarantee the interception of Storm Shadow\/SCALP in the war with Ukraine: it is a subsonic cruise missile, but it flies at low altitude, uses terrain-following flight, has a reduced radar signature, and combines multiple navigation methods with IIR terminal guidance, making it significantly harder to detect and maintain continuous radar tracking than a large high-altitude target; in addition, the route can be planned in advance to bypass air defense zones.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Therefore, even a dense layered system such as Russia\u2019s cannot provide a 100% interception rate \u2014 some missiles penetrate, particularly during massed or combined attacks, while RUSI itself notes that Storm Shadow is extremely difficult to detect and intercept because of its low-observable characteristics and design features.<\/span><\/p>\n<h2><span>SCALP Version<\/span><\/h2>\n<p><img decoding=\"async\" src=\"https:\/\/poznayu.com\/wp-content\/uploads\/2026\/09\/SCALP-EG.jpg\" class=\"aligncenter\" \/><\/p>\n<p class=\"isSelectedEnd\"><strong><span>The French SCALP-EG version<\/span><\/strong><span> (Syst\u00e8me de Croisi\u00e8re Autonome \u00e0 Longue Port\u00e9e \u2013 Emploi G\u00e9n\u00e9ral) is not an independent development or a fundamentally different missile.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Franco-British documents explicitly state that SCALP and Storm Shadow are based on an identical aerodynamic architecture, use the same TRI 60-30 engine, and are equipped with the same BROACH penetrating warhead. The different names are solely the result of the internal nomenclature standards used by the defense ministries of the two countries.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The actual differences between the British and French systems lie in the details of national integration and interfaces with launch aircraft.<\/span><\/p>\n<ul data-spread=\"false\">\n<li><span>France adapted the missile for its own combat aircraft \u2014 the Dassault Mirage 2000D and Dassault Rafale (including the naval variant), which required specialized ground mission-planning equipment and dedicated data-exchange protocols between the aircraft\u2019s onboard computers and the missile itself.<\/span><\/li>\n<li><span>The basic employment principles, flight profiles, and destructive capabilities remain fully identical to those of the British Tornado GR4 and Eurofighter Typhoon.<\/span><\/li>\n<\/ul>\n<p class=\"isSelectedEnd\"><span>Open sources and official documents contain minor discrepancies in published technical metrics.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>French government documents from the procurement period often listed the SCALP-EG warhead mass at around 400 kg, while later consolidated family references give approximately 450 kg (or 454 kg in technical specifications). French military sources have also traditionally listed a wingspan of 2.85 meters, while general catalogs round it to 3 meters.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Regarding range, Paris officially states a figure of \u201caround 400 km,\u201d which is consistent with MBDA data of more than 250 km and does not contradict independent estimates of 550\u2013560 km for full configurations.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The French arsenal, like the British one, is regularly maintained in combat-ready condition. A separate national repair and modernization program (mid-life refurbishment) was implemented for SCALP, intended to preserve the combat effectiveness of the aircraft weapon systems at least through 2030.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>In summary, modern SCALP missiles after hardware upgrades represent a weapon with the same level of resistance to electronic interference as the British SPEAR Cap 4 specification.<\/span><\/p>\n<h2><span>Technical Specifications and Design Features<\/span><\/h2>\n<p class=\"isSelectedEnd\"><span>The Storm Shadow \/ SCALP-EG family has a carefully balanced set of technical and operational characteristics, turning it into an instrument of strategic non-nuclear deterrence.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>It is important to note that the exact maximum values for flight altitude profiles and maximum range of individual missiles remain classified. To assess the system\u2019s actual capabilities, the most reliable basis is official publications from defense contractor MBDA and relevant ministries.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>Below are the system\u2019s main flight-performance and weight-and-dimension parameters, compiled from confirmed engineering data and current reference materials:<\/span><\/p>\n<table>\n<tbody>\n<tr>\n<th><strong><span>Characteristic<\/span><\/strong><\/th>\n<th><strong><span>Value<\/span><\/strong><\/th>\n<\/tr>\n<tr>\n<td><strong><span>Launch weight<\/span><\/strong><\/td>\n<td><span>1,300 kg<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Body length<\/span><\/strong><\/td>\n<td><span>5.10 m<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Cross-sectional dimensions<\/span><\/strong><\/td>\n<td><span>~630 mm (width) \u00d7 480 mm (height), non-cylindrical shape<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Wingspan<\/span><\/strong><\/td>\n<td><span>~2.85\u20133.0 m (deployed)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Engine<\/span><\/strong><\/td>\n<td><span>Microturbo TRI 60-30 turbojet (thrust ~5.4\u20135.7 kN)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Cruise speed<\/span><\/strong><\/td>\n<td><span>~Mach 0.8 (about 1,000 km\/h)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Maximum speed<\/span><\/strong><\/td>\n<td><span>~Mach 0.95 (about 1,150\u20131,160 km\/h)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Warhead<\/span><\/strong><\/td>\n<td><span>Tandem BROACH penetrating warhead (~400\u2013450 kg)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Publicly confirmed range<\/span><\/strong><\/td>\n<td><span>&gt;250 km (MBDA), ~400 km (official documents), ~550\u2013560 km (estimates for full version)<\/span><\/td>\n<\/tr>\n<tr>\n<td><strong><span>Accuracy<\/span><\/strong><\/td>\n<td><span>Meter-level (according to French Ministry of Defence data)<\/span><\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p class=\"isSelectedEnd\"><span>The system\u2019s key technological advantage is its multilayer navigation algorithm. In flight, the missile does not rely exclusively on satellite signals.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>The inertial navigation system (INS) provides basic autonomous guidance, GPS is used only for periodic correction, while the TERPROM system continuously scans the terrain beneath the missile and compares it with a digital elevation map to maintain safe ultra-low-altitude flight.<\/span><\/p>\n<p class=\"isSelectedEnd\"><span>During the final terminal phase, the imaging infrared system (IIR) activates: it autonomously recognizes the contours of the preselected target, ignoring thermal decoys and enemy electronic warfare measures, enabling a direct hit on a vulnerable point of the structure.<\/span><\/p>\n<div contenteditable=\"false\">\n<hr \/>\n<\/div>\n<p class=\"isSelectedEnd\"><span>As for the specifications, the basic figures are listed above in the table. Below, we will examine the Storm Shadow specifications in greater detail and provide some commentary:<\/span><\/p>\n<ol data-spread=\"false\" start=\"1\">\n<li><strong><span>Type:<\/span><\/strong><span> air-launched cruise missile in the air-to-surface \/ stand-off \/ deep-strike class.<\/span><\/li>\n<li><strong><span>Manufacturer:<\/span><\/strong><span> MBDA; original development \u2014 Matra BAe Dynamics.<\/span><\/li>\n<li><strong><span>Launch weight:<\/span><\/strong><span> <\/span><strong><span>1,300 kg<\/span><\/strong><span>. This is one of the most consistently confirmed characteristics.<\/span><\/li>\n<li><strong><span>Length:<\/span><\/strong><span> <\/span><strong><span>5.10 m<\/span><\/strong><span>.<\/span><\/li>\n<li><strong><span>Cross-sectional dimensions:<\/span><\/strong><span> approximately <\/span><strong><span>630 \u00d7 480 mm<\/span><\/strong><span> \u2014 width \u00d7 height of the body. This is an important clarification: the widely used online designation \u201c480 mm diameter\u201d is incorrect because the body has a low-observable non-cylindrical shape. Open references citing Jane\u2019s list a width of 630 mm and a height of 480 mm.<\/span><\/li>\n<li><strong><span>Wingspan:<\/span><\/strong><span> about <\/span><strong><span>3.0 m<\/span><\/strong><span> when deployed.<\/span><\/li>\n<li><strong><span>Aerodynamic configuration:<\/span><\/strong><span> folding wings, a compact low-observable body, and control surfaces. Open reference data lists <\/span><strong><span>6 control surfaces \u2014 4 vertical and 2 horizontal<\/span><\/strong><span>.<\/span><\/li>\n<li><strong><span>Propulsion system:<\/span><\/strong><span> <\/span><strong><span>Microturbo TRI 60-30<\/span><\/strong><span> turbojet.<\/span><\/li>\n<li><strong><span>Engine thrust:<\/span><\/strong><span> typically listed at about <\/span><strong><span>5.4 kN<\/span><\/strong><span>; technical tables for the TRI 60-30 family show <\/span><strong><span>5.7 kN<\/span><\/strong><span> depending on the engine operating mode\/rating. Therefore, 5.4 kN is the more appropriate figure for the configuration installed on the missile according to publicly available sources.<\/span><\/li>\n<li><strong><span>Speed:<\/span><\/strong><span> subsonic.<\/span><br \/>\n<strong><span>Cruise:<\/span><\/strong><span> about <\/span><strong><span>Mach 0.8<\/span><\/strong><span>.<\/span><br \/>\n<strong><span>Maximum speed cited in current open references:<\/span><\/strong><span> about <\/span><strong><span>Mach 0.95<\/span><\/strong><span>.<\/span><\/li>\n<li><strong><span>Speed in km\/h:<\/span><\/strong><span> approximately <\/span><strong><span>1,000 km\/h<\/span><\/strong><span> at M0.8; depending on altitude and conditions, sources give a maximum of about <\/span><strong><span>1,150\u20131,160 km\/h<\/span><\/strong><span> at M0.95.<\/span><\/li>\n<li><strong><span>Range:<\/span><\/strong><span> this is the main source of confusion.<\/span><br \/>\n<strong><span>Official MBDA figure:<\/span><\/strong><span> <\/span><strong><span>more than 250 km<\/span><\/strong><span>.<\/span><br \/>\n<span>French parliamentary materials for SCALP\/Storm Shadow indicate around <\/span><strong><span>400 km<\/span><\/strong><span>.<\/span><br \/>\n<span>Current open technical references give approximately <\/span><strong><span>550\u2013560 km<\/span><\/strong><span> for the full configuration.<\/span><\/li>\n<\/ol>\n<p class=\"isSelectedEnd\"><span>Therefore, the correct wording is: the publicly confirmed range of the family starts at 250+ km; for full national configurations, open sources usually cite approximately 400\u2013560 km. The exact maximum range of an individual missile has not been disclosed.<\/span><\/p>\n<ol data-spread=\"false\" start=\"13\">\n<li><strong><span>Flight altitude:<\/span><\/strong><span> <\/span><strong><span>very low, with terrain hugging<\/span><\/strong><span> (terrain hugging \/ terrain following). The exact maximum and minimum altitudes have not been officially disclosed. Older technical sources give approximately <\/span><strong><span>30\u201340 m<\/span><\/strong><span> for the very-low-altitude\/attack segment; higher cruise altitudes are cited for some flight modes.<\/span><\/li>\n<li><strong><span>Navigation system:<\/span><\/strong><span> combined:<\/span><\/li>\n<\/ol>\n<ul data-spread=\"false\">\n<li><strong><span>INS<\/span><\/strong><span> \u2014 inertial navigation system;<\/span><\/li>\n<li><strong><span>GPS<\/span><\/strong><span>;<\/span><\/li>\n<li><strong><span>Terrain Reference Navigation \/ TERPROM<\/span><\/strong><span> \u2014 terrain-profile navigation.<\/span><\/li>\n<\/ul>\n<ol data-spread=\"false\" start=\"15\">\n<li><strong><span>Terminal guidance:<\/span><\/strong><span> <\/span><strong><span>IIR \u2014 Imaging Infrared<\/span><\/strong><span>, an infrared imaging system. Near the target, the missile compares the acquired image with preloaded reference information about the target.<\/span><\/li>\n<li><strong><span>Target recognition:<\/span><\/strong><span> automated matching of the target image during the terminal phase. This distinguishes it from a missile that simply follows preprogrammed GPS coordinates.<\/span><\/li>\n<li><strong><span>Employment mode:<\/span><\/strong><span> <\/span><strong><span>fire-and-forget<\/span><\/strong><span> \u2014 after launch, the core concept provides autonomous flight according to a preplanned mission.<\/span><\/li>\n<li><strong><span>Retargeting after launch:<\/span><\/strong><span> for the original missile architecture, it is publicly described as unavailable; mission data are prepared before launch. The capabilities of upgraded systems have not been fully disclosed publicly.<\/span><\/li>\n<li><strong><span>Warhead:<\/span><\/strong><span> <\/span><strong><span>BROACH \u2014 Bomb Royal Ordnance Augmenting Charge<\/span><\/strong><span>, a multi-component tandem penetrating warhead.<\/span><\/li>\n<li><strong><span>Warhead mass:<\/span><\/strong><span> typically <\/span><strong><span>about 450 kg<\/span><\/strong><span>; technical literature lists <\/span><strong><span>454 kg<\/span><\/strong><span> in some cases.<\/span><\/li>\n<li><strong><span>BROACH principle:<\/span><\/strong><span> a precursor charge\/penetrator acts ahead of the main penetrating warhead, creating a channel through the barrier; the main warhead then passes inside and detonates with a delay.<\/span><\/li>\n<li><strong><span>Warhead type:<\/span><\/strong><span> blast\/penetrator \u2014 a blast-penetrating warhead primarily intended for hardened targets.<\/span><\/li>\n<li><strong><span>Officially stated penetration capability for the French SCALP-EG:<\/span><\/strong><span> <\/span><strong><span>more than 1 m of concrete<\/span><\/strong><span>. This is an official French specification and is therefore substantially more reliable than internet estimates claiming several meters.<\/span><\/li>\n<li><strong><span>Accuracy:<\/span><\/strong><span> French official materials characterize it as <\/span><strong><span>meter-level<\/span><\/strong><span>. A specific modern CEP figure has not been disclosed in public official sources.<\/span><\/li>\n<li><strong><span>Low observability:<\/span><\/strong><span> <\/span><strong><span>low observable \/ reduced radar signature<\/span><\/strong><span> design; the specific RCS is not published.<\/span><\/li>\n<li><strong><span>Weather conditions:<\/span><\/strong><span> designed for operation <\/span><strong><span>day and night, in all weather conditions<\/span><\/strong><span>.<\/span><\/li>\n<li><strong><span>Primary target classes:<\/span><\/strong><span> hardened bunkers, command facilities, infrastructure, airfield facilities, energy facilities, storage sites, and other fixed high-value targets.<\/span><\/li>\n<li><strong><span>Standard carriers in the British system:<\/span><\/strong><br \/>\n<strong><span>Panavia Tornado GR4<\/span><\/strong><span> and <\/span><strong><span>Eurofighter Typhoon<\/span><\/strong><span>.<\/span><\/li>\n<li><strong><span>Other family integrations:<\/span><\/strong><span> Mirage 2000, Rafale, Tornado, Typhoon; some export users have their own integration variants.<\/span><\/li>\n<li><strong><span>Ukrainian integration:<\/span><\/strong><span> the missile has been integrated with the <\/span><strong><span>Su-24<\/span><\/strong><span>, but this is not the original factory platform for the family and instead represents a separate adaptation.<\/span><\/li>\n<li><strong><span>Entry into service:<\/span><\/strong><span> the British Storm Shadow entered service in the early 2000s; its first combat use was in the 2003 Iraq War.<\/span><\/li>\n<\/ol>\n<p><span>Franco-British documents explicitly state that SCALP-EG and Storm Shadow share the same architecture; the initial differences were mainly related to national requirements, aircraft interfaces, and ground equipment.<\/span><\/p>\n<div style='text-align:right' class='yasr-auto-insert-visitor'><\/div>","protected":false},"excerpt":{"rendered":"<p>The experience of military conflicts in the late twentieth century, particularly the 1991 Multinational Force operation in Iraq, demonstrated a [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":863,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"site-sidebar-layout":"default","site-content-layout":"","ast-site-content-layout":"default","site-content-style":"default","site-sidebar-style":"default","ast-global-header-display":"","ast-banner-title-visibility":"","ast-main-header-display":"","ast-hfb-above-header-display":"","ast-hfb-below-header-display":"","ast-hfb-mobile-header-display":"","site-post-title":"","ast-breadcrumbs-content":"","ast-featured-img":"","footer-sml-layout":"","ast-disable-related-posts":"","theme-transparent-header-meta":"default","adv-header-id-meta":"","stick-header-meta":"","header-above-stick-meta":"","header-main-stick-meta":"","header-below-stick-meta":"","astra-migrate-meta-layouts":"set","ast-page-background-enabled":"default","ast-page-background-meta":{"desktop":{"background-color":"var(--ast-global-color-5)","background-image":"","background-repeat":"repeat","background-position":"center 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