R-25 Vulkan

R-25 Vulkan
A telemetry-equipped R-25 on display at the Aviation Museum - Belgrade
Type	Surface-to-air missile (SAM)
Place of origin	Yugoslavia
Production history
Designer	Obrad Vučurović at Military Technical Institute Belgrade
Designed	1958 onwards
Manufacturer	SOKO
No. built	12
Specifications
Mass	1,413 kg (3,115 lb) at launch
Length	8.10 m (26.6 ft) total length at launch
length	5.24 m (17.2 ft) missile without booster rockets
Diameter	350 mm (14 in)
Engine	RM-1000B sustainer 11.77 kN (2,650 lbf) thrust - sustainer, 245.25 kN (55,130 lbf) thrust - boosters
Propellant	liquid fuel sustainer, solid-fuelled boosters
Operational range	30 km (19 mi)
Flight altitude	20 km (12 mi)
Maximum speed	M2.5
Guidance system	Radar initially with infra-red terminal guidance
Steering system	Aerodynamic

The R-25 Vulkan (Serbian: Вулкан) was a surface-to-air missile (SAM) designed by Serbian engineer Obrad Vučurović and built in the Socialist Federal Republic of Yugoslavia (SFRY) 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.[1] Designated the R-25 Vulkan (Volcano), 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.[1]

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.[1] The development of the launcher and radar system was inspired by the Japanese Kappa meteorological sounding rocket imported into Yugoslavia.[2] 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.[1] For operational use, there existed the possibility of using more sophisticated radar equipment,[1] and for terminal guidance the missile would switch to independent homing by infrared sensors in its nose cone.[1] The advanced guidance system of the R-25 was automatic after launch with no further operator input needed.[1]

Use

The first launch of the missile was conducted in November 1962, revealing problems with the liquid-fueled sustainer rocket motor.[1] Concurrently, with the R-25 testing in 1962 the SFRY acquired S-75 Dvina (Russian: С-75; NATO reporting name: SA-2 Guideline), missile systems from the Soviet Union.[1] As such, by the end of 1964 the decision was made to abandon the Vukan project that produced a total of twelve missiles.[1] The knowledge and experience gained during this project were later incorporated into other projects for production of other armaments for the Yugoslav People's Army (JNA).[1]

Survivors

A single R-25 Vulkan missile is preserved at the Museum of Aviation Museum in Belgrade; intended for in-flight testing, the warhead has been replaced by measuring and telemetry equipment.[1]

External links

• Seven-boostered version images

References

1. "Соко Вулкан (ракета З-В)". Belgrade Museum of Aviation. Archived from the original on May 5, 2014. Retrieved January 18, 2013.
2. Ichiro Matsuo (July 16, 2012). "Japan rocket technologies misused by Yugo military in 1960s". Asahi Shimbun. Archived from the original on October 21, 2012. Retrieved January 18, 2013.