It consists of extendable probe (mechanical), switching unit,canister, grenade ejection unit, rocket motor, retarding tail unit with parachute.
Launched from single tubular launcher
Calibre - 340 mm
Weight 100 kg, Fuel- 38 kg propylene oxide
Range - Anywhere from 250 to 500 m
Stabilized by fins of RTU and parachute
A/T NDMK-I mine clearance - 16 m dia.
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