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Technical Specifications of KHAN Missile

Diameter 610 mm
Maximum Range 280 km
Minimum Range 80 km
Weight 2500 kg
Guidance • GNSS aided INS
• Only INS
CEP • ≤ 10 m GNSS Aided INS
• ≥ 150 m Only INS (at Max Range)
Control Aerodynamical Control with Electromechanical Actuation System
Propellant Type Composite Solid
Warhead Type High Explosive - Pre Fragments
Warhead Weight 470 kg
Warhead Effective Radius ≥ 100 m
Fuze Type Proximity and Point Detonating
NATO Stock Number 140 27 065 2841

TRG-122 GUIDED

ROCKET Technical Specifications of the

TRG-122 Guided Rocket

The Artillery Guided Rocket TRG-122, designed and Diameter 122 mm
produced by Roketsan, can provide mass firepower Maximum Range 35 km
on High Payoff Targets with coverage between 16 km
and 35 km range, perfect accuracy and minimum Minimum Range 16 km
dispersion. TRG-122 provides timely, accurate and Weight 72 kg
effective fire support to manoeuvre forces.
Guidance Global Navigation Satellite System
TRG-122 can be launched from T-122 SAKARYA (GNSS)
Multi Launch Rocket System, Multi Caliber Launcher Control Aerodynamic Control with
(MCL) Weapon System and other compatible Electromechanical Actuation System
platforms with suitable interfaces for integration.
CEP ≤ 15 m
Against adverse weather conditions, TRG-122 is Propellant Type Composite Solid
placed inside a canister and is stored, transported, Warhead Type HE- Fragmentation (Steel Ball)
loaded and launched in Missile in Canister (MIC)
configuration. Warhead Weight 13 kg
Warhead Effective Radius ≥ 50 m
TRG-122 can be used against sensitive targets
requiring pinpoint accuracy while minimizing Fuze Type Proximity and Point Detonating
collateral damage.

Potential targets for TRG-122 are:

• Harbors and Airfields
• Assembly Areas (Vehicles and/or Personnel)
• Accurately Located Targets
• Logistic Facilities
• Enemy Artillery and Air Defense Artillery (ADA)
Systems
• C3 Systems
• Caves and Havens

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