Roketsan

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Documents

Roketsan Tayfun ballistic missile brochure (PDF)

Strategic missiles

Turkey In development

Roketsan

TAYFUN Block 4

Enlarged, longer-range evolution of Turkey's Tayfun ballistic missile, unveiled in 2025 with claimed hypersonic terminal capability. Range and speed figures are manufacturer or state-sourced and not independently verified.

Compiled from public sources ·primary reference ↗ ·last verified 2026-07-04

Procurement snapshot

Availability & export

Türkiye export-licensed

SSB-administered; growing export programme, some Western sub-component dependencies.

Channel: Direct commercial / G2G

Development status

Operator data not public

Status: announced.

Lifecycle cost (est.)

No public unit price to model from. Why so few systems publish one →

Interoperability

No standardised NATO calibre / datalink detected in public specs.

Derived guidance from public data, export regime by country of origin, lifecycle from the GAO ~30% acquisition rule. Verify eligibility, pricing and offsets with the manufacturer and your acquisition authority.

Full specifications

Performance

Speed, range, altitude and engagement capability.

Performance specifications
Range Maximum distance: ferry range for aircraft, operational range for vehicles, maximum engagement distance for missiles. Higher means more standoff or persistence.	1,000 km Bottom 3% of its class

Firepower

Armament, payload and guidance.

Firepower specifications
Warhead type Blast-fragmentation, shaped charge (HEAT), penetrator, thermobaric or nuclear-capable.	HE or fragmentation
Guidance How the weapon finds its target: inertial, GPS/GLONASS, active/semi-active radar, infrared, laser, TV, wire.	GPS/GLONASS-aided INS, INS-only

Physical

Dimensions, weight and crew.

Physical specifications
Length Overall length including gun/probe where applicable.	10 m
Width Overall width, matters for rail/road transport of vehicles.	0.94 m
Combat weight Fully loaded weight. Lighter eases transport and bridging limits; heavier often means more armor.	7,200 kg

Propulsion

Engine, power and fuel.

Propulsion specifications
Propulsion type Turbofan, turboshaft, diesel, gas turbine, solid-fuel rocket, ramjet…	composite solid propellant

Specifications compiled from public Roketsan and reference sources ↗. Published defense figures are approximations, treat comparisons as directional. Last verified 2026-07-04.

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