open source file
ATMACA
ROKETSAN's anti-ship cruise missile.
Scale comparison
Schematic model
The schematic look is deliberate: a photorealistic render would claim an accuracy we do not have. There is no cutaway, no exploded view and no internal component layout, because we have no sourced data on internal geometry. Labels name external sections only and each carries its own confidence level. The model is scaled from the published length and diameter; the proportions of the body and fins are not published figures, and the origin of each is set out in the shape record below. This is not a technical drawing.
The model is scaled from published measurements. The ratios that determine its shape are not published figures; each one states below where it came from. This is a statement of origin, not a confidence level.
15 measured · 0 reading · 2 chosen
- Nose sectionmeasured
Nose cap. The body reaches full diameter 74 px aft of the tip, 6% of the body length. A blunt radome rather than a sharp ogive.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- End of full-diameter sectionmeasured
The body holds full diameter all the way to the aft face; the drawing shows no taper. The short piece behind the tail belongs to the interface, not the body.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Boattailmeasured
No boattail: the upper and lower body edges stay parallel to the aft face.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin countmeasured
Four fins at the tail.
sourceseen: 2026-09-11
projection check: A count does not depend on projection: four surfaces are four in any view. The number was taken from the manufacturer’s 3D illustration in the same catalogue; the top-view drawing shows the outline of the lateral pair.
- Fin root chordmeasured
The root chord measures 113 px at the body axis. The 73 px visible in the drawing is the chord at the body surface; the model roots the panel on the axis, so both edges were extrapolated linearly inward. The previous chosen value was 14%, the measured one is 9.2%.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin tapermeasured
The tip chord measures 36 px, roughly a third of the root chord at the axis.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin spanmeasured
The fin tip sits 1.98 radii from the body axis. The top view shows the lateral pair at full span; the roll angle of the set cannot be read from the drawing, so the four surfaces are taken as symmetric.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin trailing-edge rakemeasured
The trailing edge holds the same station across the whole span: x = 569 px from root to tip, within one pixel. So it is perpendicular to the body axis. The leading edge moves from 642 to 605, and the sweep follows from the three ratios.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin trailing-edge positionmeasured
The fin trailing edge does not sit at the very tail but 2% forward of it.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Wing countmeasured
Four wings at mid-body. These are the system’s dominant surfaces and were not drawn at all in the previous version.
sourceseen: 2026-09-11
projection check: A count does not depend on projection: four surfaces are four in any view. The number was taken from the manufacturer’s 3D illustration in the same catalogue; the top-view drawing shows the outline of the lateral pair.
- Wing root chordmeasured
The root chord measures 328 px at the body axis. What the drawing shows at the body surface is 229 px; both edges were extrapolated linearly inward. Roughly three times the fin chord.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Wing tapermeasured
The tip chord measures 65 px, a fifth of the root chord at the axis. The wing tapers sharply from root to tip.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Wing spanmeasured
The wing tip sits 2.74 radii from the body axis, clearly outboard of the fin tip. The top view shows the lateral pair at full span.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Wing trailing-edge rakemeasured
Unlike the fin, the trailing edge is not perpendicular: it moves toward the nose at the tip. It sits at x = 951 px at the root and 1100 px at the tip, 149 px forward across a span of 143.85 px. The leading edge moves the other way, from 1279 to 1165.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Wing trailing-edge positionmeasured
At the axis the wing trailing edge sits at 66.9% of body length from the nose; the wing occupies the middle section.
sourceseen: 2026-09-11
projection check: The drawing was directly checked for orthographic projection: body width holds at 105.2 px ± 1.4 px (1.4%) along its length, the body axis does not drift, and the upper and lower surfaces mirror within one pixel. A perspective view would taper toward the far end and the axis would wander.
- Fin thicknesschosen
Thickness as a fraction of LOCAL chord. It cannot be read from a top view, where the surface lies in its own plane. A thin plate was chosen to keep the schematic language.
- Wing thicknesschosen
Thickness as a fraction of LOCAL chord. It cannot be read from a top view. Chosen thinner than the fin; a thin plate is reasonable for a folding surface.
Technical data and sources
| Field | ATMACA |
|---|---|
| Length different statements | 4.3 – 5.2mofficialROKETSAN ATMACA product web page · Sep 11, 2026declared5.2mofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439…declared |
| Diameter | 370mmofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439… |
| Mass contradiction | < 750kgofficialROKETSAN ATMACA product web page · Sep 11, 2026declared750kgofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439…declared< 800kgpressSavunma Sanayi, 4 Nov 2019 · Sep 11, 2026declared · 2019 statement |
| Range different scope | 250kmofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439…declared> 200kmofficialSSB Chair Ismail Demir statement, 4 Jul 2020 · Sep 11, 2026measured in a test · 2020 statement |
| Warhead weight contradiction | 220kgofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439…declared250kgpressNaval News, 5 Feb 2021 · Sep 11, 2026declared · 2021 statement |
| Guidance | Inertial navigation, anti-jam GNSS, barometric and radar altimeter; active radar seekerofficialROKETSAN ATMACA PDF catalogue, 2024 catalogue · Sep 11, 2026 · digest c7163fec0439… |
| Propellant | Turbojet (Kale KTJ-3200)pressTRT World, 10 Mar 2024 · Sep 11, 2026 |
Programme timeline
Project startpress
Started under ROKETSAN to meet the Turkish Naval Forces' surface-to-surface cruise missile requirement.
Daily Sabah, 5 Jul 2020Serial production contractofficial
Serial production contract signed between SSB and ROKETSAN.
Naval News, 5 Feb 2021200 km-plus target hitofficial
A launch in the Black Sea hit a target beyond 200 km.
SSB Chair Ismail Demir statement, 4 Jul 2020IOC testpress
Initial operational capability achieved with a live-warhead test.
Naval News, 5 Feb 2021Serial production startedofficial
ROKETSAN CEO Murat İkinci announced that serial production began in the first half of 2021.
ROKETSAN, 17 Aug 2021Land-based test launchpress
Fired from land against a sea target; treated as the first step toward KARA ATMACA.
DefenceTurk, 2 Jul 2022First submarine launchpress
Encapsulated launch test conducted from TCG Preveze (S-353).
Naval News, 13 Mar 2025
Range envelope
Drag the reference point to move it. The rings are geodesic projections of published range figures; they do not show a flight profile or operational use.
Compiled from publicly available sources. Not an official publication and not affiliated with the manufacturer.