R-25 Vulkan
The R-25 Vulkan was a surface-to-air missile designed by Serbian engineer Obrad Vučurović and built in the Socialist Federal Republic of Yugoslavia in the late 1950s, early 1960s.
Development
The mid-1950s saw the emergence of viable SAMs for the purpose of air defence. Due to their inability to import foreign SAM systems, in 1958 Yugoslavia initiated a program to develop an indigenous missile at the Belgrade Military Technical Institute. Designated the R-25 Vulkan, this completely original Yugoslavian design brought together a team of experts led by engineer Obrad Vučurović to design the missile, with the prototypes being made in the SOKO aircraft factory in Mostar.Two versions of the missile were developed: one that had a booster-rocket engine with seven rockets and a second one with four rockets. Although, initial prototypes used a liquid fuel rocket engine developed for a rocket-powered torpedo, later operational production missiles would use a solid-fueled engine with twice the thrust. The development of the launcher and radar system was inspired by the Japanese Kappa meteorological sounding rocket imported into Yugoslavia. The target detection and information collection system was supplied by Yugoslav-made OAR M-61 “Fruška Gora” S-Band surveillance and acquisition radar, and in-course guidance was supplied by a British No. 3 Mk. 7 aiming radar. For operational use, there existed the possibility of using more sophisticated radar equipment, and for terminal guidance the missile would switch to independent homing by infrared sensors in its nose cone. The advanced guidance system of the R-25 was automatic after launch with no further operator input needed.