An airburst projectile for countering an unmanned aerial vehicle (UAV) comprising: an ogive connected to a fuze assembly , the fuze assembly is then connected to a shell ; and the fuze assembly comprises a programmable fuze and an electric detonator; wherein the ogive houses: a spinner (140,140a-140d), wherein the spinner (140,140a-140d) comprises a rear annular plate being connected along an inner annular edge to a sleeve , and a plurality of partition plates extending radially from the sleeve and being in contact with a face of the rear annular plate , so that a space between adjacent radial partition plates and the rear annular plate forms each compartment and a streamer , in a coiled up state, is disposed in each compartment ; wherein the spinner (140,140a-140d) and the fuze assembly are located forward of the electric the airburst projectile is configured to be fired into a flight path of the UAV, such that when the ogive is burst open by activating the electric detonator, the spinner (140,140a-140d) is ejected, causing the streamers to disperse and the streamers to open up from the coiled up state, thus creating a streamer cloud in the flight path of the UAV. an ogive connected to a fuze assembly , the fuze assembly is then connected to a shell ; and the fuze assembly comprises a programmable fuze and an electric detonator; wherein the ogive houses: a spinner (140,140a-140d), wherein the spinner (140,140a-140d) comprises a rear annular plate being connected along an inner annular edge to a sleeve , and a plurality of partition plates extending radially from the sleeve and being in contact with a face of the rear annular plate , so that a space between adjacent radial partition plates and the rear annular plate forms each compartment and a streamer , in a coiled up state, is disposed in each compartment ; wherein the spinner (140,140a-140d) and the fuze assembly are located forward of the electric the airburst projectile is configured to be fired into a flight path of the UAV, such that when the ogive is burst open by activating the electric detonator, the spinner (140,140a-140d) is ejected, causing the streamers to disperse and the streamers to open up from the coiled up state, thus creating a streamer cloud in the flight path of the UAV. wherein the ogive houses: a spinner (140,140a-140d), wherein the spinner (140,140a-140d) comprises a rear annular plate being connected along an inner annular edge to a sleeve , and a plurality of partition plates extending radially from the sleeve and being in contact with a face of the rear annular plate , so that a space between adjacent radial partition plates and the rear annular plate forms each compartment and a streamer , in a coiled up state, is disposed in each compartment ; wherein the spinner (140,140a-140d) and the fuze assembly are located forward of the electric the airburst projectile is configured to be fired into a flight path of the UAV, such that when the ogive is burst open by activating the electric detonator, the spinner (140,140a-140d) is ejected, causing the streamers to disperse and the streamers to open up from the coiled up state, thus creating a streamer cloud in the flight path of the UAV. <EOS>