9M337 Sosna-R
View on WikipediaThe 9M337 Sosna-R (Pine) (SA-X-25)[1][2] is a Russian radar and laser-guided supersonic (Mach 2.6) two-stage missile. It is used in Sosna-R short range air defense missile system designed to protect military units from air attacks in all types of combat situations, including during march.
Key Information
In 2017, official tests of the newest air defense missile system Bagulnik (domestic variant which is currently named Strela-10ML) were successfully completed.[3][4][5]
Description
[edit]It was developed by KB Tochmash as a successor to 9K35 Strela-10, and is a cheaper alternative to the Tor missile system and Pantsir-S1. Designed to work in passive mode with the help of different imaging systems (thermal camera, TV camera) and a laser rangefinder in order to find and engage a target, Sosna-R is able to operate effectively under the control of various types of old, modern and prospective battery command posts, the most preferable of which is the FPU "Assembly-M1-2" (9S80M1-2) and is resistant to jamming. It uses a tracked SAM launcher with 12 missiles of 10 km range and altitude of 5 km, based on the MT-LB vehicle. Those 12 missiles can be reloaded in 12 minutes.[6][7] The serial production version is based on the BMP-3 IFV.[8][9] The Sosna can also deliver fire while on the move.[10] The system has a crew of two: the driver and gunner.
The system is armed with 12 9M340 missiles that are held in their transport-launch containers and arranged in two banks of six.[11] Sosna-R beam rider 38 kg missiles are two-stage, capable of destroying aircraft, helicopters, cruise missiles, aerial bombs, small-sized air attack weapons including elements of high-precision weapons and light armored vehicles. The missile can change direction mid-flight.[12][13] It also has a combined impact/proximity laser fuze. Its payload is made up of two warheads weighing a total of 7 kg. The fragmented-rod warhead is designed for proximity detonation when flying close to the target, while the armor-piercing/fragmentation (AP-Frag) warhead goes off on impact.[14] The system has high resistance to jamming and besides its passive mode of operation it can be equipped with an additional small-size acquisition radar.
The Palma anti-aircraft artillery system features integrated armament that comprises eight Sosna-R precision surface-to-air missiles with laser beam guidance and two AO-18KDE rapid-fire guns. As a defense component, the Palma is designated to defend both ships and naval bases, coastal infrastructure and aerodromes, and also other vital facilities.[15]
Range
[edit]Within 8–10 (≤ 20) km.

Variants
[edit]- Sosna A weapon module for MBT, IFV, APC, AFV
- Sosna RA for AFV, MBT, IFV, APC
- Palash CIWS
- Palma CIWS - the deliveries of the systems to the Russian Navy and foreign navies started in 2011.[16][17]
- Ptitselov CIWS is an air transportable version based on the BMD-4M chassis and it can also be dropped by parachute[18]
Operators
[edit]Current operators
[edit]- Palma-SU CIWS used on Gepard 3.9 frigates.
Potential operator
[edit]- Potential Palma CIWS acquisition reported.[19]
See also
[edit]References
[edit]- ^ "Sosna short-range air defense missile system".
- ^ "9K338 9M342 Igla-S / SA-24 Grinch".
- ^ "Новейший ЗРК "Багульник" успешно прошел испытания". vesti.ru. Retrieved 21 January 2019.
- ^ ШАГвперед (8 April 2018). "Новейший российский ЗРК "Багульник"". Retrieved 21 January 2019 – via YouTube.
- ^ "Tłumacz Google".
- ^ Administrator. "Sosna short-range air defense missile system technical data sheet specifications pictures video 11312155 - Russia Russian missile system vehicle UK - Russia Russian army military equipment vehicles UK". www.armyrecognition.com.
- ^ Pike, John. "9K338 9M342 Igla-S / SA-24 Grinch".
- ^ "Army 2019: Nudelman displays Sosna missile air defense system and BMP-3 with add-on armor | Army-2019 News Russia Online Show Daily Media Partner | Defence security military exhibition 2019 daily news category".
- ^ "Janes | Latest defence and security news".
- ^ "Russian hi-tech firm showcases latest Sosna short-range air defense missile system". TASS. Retrieved 21 January 2019.
- ^ "Army 2018: Russia unveils Sosna SHORAD system production version - Jane's 360". www.janes.com. Retrieved 21 January 2019.
- ^ "SOSNA-R Air defense System". defense-update.com. Archived from the original on 2018-01-06. Retrieved 2018-01-05.
- ^ "Sosna-R". www.deagel.com. Retrieved 21 January 2019.
- ^ "Russian Sosna air defense missile system unveiled at Army-2018 | Army-2018 News Russia Online Show Daily | defense security exhibition 2018 pictures gallery". Armyrecognition.com. 2018-08-21. Retrieved 2019-01-21.
- ^ "Hi-tech firm delivers ten seaborne air defense systems to Russian Navy and foreign fleets".
- ^ "Janes | Latest defence and security news".
- ^ "ЦАМТО / / Глава «Рособоронэскпорта» Александр Михеев: комплекс ПВО «Пальма» впервые интегрируют на иностранный корабль".
- ^ "Russia developed parachute-dropped Ptitselov SAM for Airborne units". 15 May 2023.
- ^ "Egypt Navy, Almaz-Antey, and Palma air defense systems". Tactical Report. 2021-09-28. Retrieved 2021-12-31.
9M337 Sosna-R
View on GrokipediaDevelopment
Origins and Design Phase
The 9M337 Sosna-R missile system emerged as a direct successor to the aging 9K35 Strela-10 short-range air defense system, which faced significant limitations in engaging modern aerial threats such as low-flying cruise missiles, unmanned aerial vehicles, and precision-guided munitions due to its outdated infrared guidance and limited range and speed capabilities.[4][3] Developed to address these shortcomings, the Sosna-R was conceived to provide enhanced protection for ground forces against evolving air attack means, emphasizing mobility and effectiveness in contested environments.[4][5] Development of the Sosna-R began around 2005 under the auspices of the Nudelman Precision Machine-Building Design Bureau (KB Tochmash), a subsidiary of High Precision Systems within the Rostec State Corporation, with the system unveiled at the Army-2018 forum and preliminary operational capability achieved around 2011.[3][5][4] The project focused on creating a supersonic, two-stage solid-fuel missile design optimized for short-range air defense, prioritizing lightweight construction and high maneuverability to counter fast-moving targets.[3] Key engineering efforts centered on achieving a missile speed exceeding Mach 2.5 while maintaining a launch weight of 42 kg, which presented challenges in balancing propulsion efficiency, structural integrity, and aerodynamic stability during the boost and sustain phases.[3][1] Central to the design phase were goals to bolster electronic warfare resilience through an advanced electro-optical guidance system resistant to jamming, enabling all-weather operations via combined radio-command and laser-beam homing for precise target acquisition even in low-visibility conditions.[4] The system was engineered for fire-on-the-move capability, allowing launches from tracked vehicles such as the MT-LB chassis while in motion, thereby supporting dynamic battlefield maneuvers without compromising accuracy.[4] These innovations aimed to integrate seamlessly with existing mechanized units, providing a cost-effective upgrade over more complex systems like the Tor or Pantsir-S1 while retaining operational simplicity.[4] Early prototypes underwent iterative refinements to optimize the dual-stage configuration, where the initial booster provided rapid acceleration and the sustainer ensured extended powered flight, addressing hurdles in miniaturizing components for reduced overall system weight and improved launcher compatibility.[3]Testing and Entry into Service
The development of the 9M337 Sosna-R missile system as a successor to the Strela-10 involved rigorous testing phases, with official evaluations completed in 2017 under the Bagulnik program, later redesignated as Strela-10ML. These tests encompassed live-fire trials targeting simulated aircraft and helicopters to validate the system's interception capabilities in operational scenarios.[6] Following preliminary tests, state trials began in the summer of 2015 at Russian testing grounds, with completion announced in 2019, leading to certification by the Russian Ministry of Defense. The certification process highlighted the system's reliability across diverse terrains, including rough and mobile environments, as well as its resilience in electronic warfare conditions through jam-protected electro-optical guidance.[7][8] The Sosna-R entered service with the Russian armed forces in 2019, following the Ministry of Defense's decision to adopt the system for short-range air defense roles. Serial production commenced in 2018, with full-scale deliveries authorized in 2022 by High Precision Systems, enabling broader integration into military units.[6][8][4] Initial deployments focused on motorized and airborne units, such as the Ptitselov variant mounted on BMP-3 vehicles for Russian Airborne Forces. Crew training protocols were established for a two-person operation, consisting of a driver and a gunner, emphasizing rapid setup, target acquisition, and fire control in dynamic battlefield conditions.[6]Design and Components
Missile Configuration
The 9M337 Sosna-R employs a two-stage solid-fuel rocket configuration, where the initial boost stage provides rapid acceleration post-launch, and the sustainer stage maintains propulsion during mid-course flight. This architecture incorporates a detachable booster motor, separating after initial burn to reduce mass and enhance efficiency, while enabling the missile to perform aggressive maneuvers with lateral overloads up to 52 g.[9][2][10] Physically, the missile measures approximately 2.3 meters in length during flight (2.4 meters when housed in the transport-launch container) and has a body diameter of 72 mm, expanding to 132 mm with the booster stage attached. Its total weight at launch, including the container, is around 42 kg, making it compact for integration into mobile platforms while supporting vertical launch from sealed canisters.[9][2] The warhead is a dual-mode design totaling approximately 7 kg, featuring a fragmented-rod configuration for proximity airburst effects via laser proximity fuse and an armor-piercing fragmentation mode for direct impact detonation. This setup, triggered by a combined laser-impact fuze, optimizes lethality against aerial targets by adapting to engagement scenarios.[1][9] Aerodynamic control is provided by fixed tail fins on the sustainer stage, ensuring stability during supersonic flight following booster separation.[3]Guidance and Launcher Systems
The 9M337 Sosna-R employs a hybrid guidance system using radio-command in the initial phase after launch, transitioning to semi-active laser beam-riding for the main flight phase.[3] This approach allows the missile to ride along a laser beam directed at the target, providing precise control while minimizing susceptibility to electronic countermeasures. The system's jam-resistant acquisition is facilitated by passive sensors that avoid active emissions during initial targeting.[11] The sensor suite integrates an optical-electronic station equipped with a passive thermal imaging and television (TV) camera for all-weather, day-night operation, alongside a laser rangefinder for accurate distance measurement.[3] An accompanying radar supports detection of airborne threats and cueing for the passive optical systems, which operate in a sector-scanning mode to track multiple targets autonomously.[3] This configuration emphasizes low observability, as the system can function without radar emissions in passive mode to reduce vulnerability to anti-radiation threats.[9] The launcher is mounted on a tracked vehicle chassis, typically the MT-LB multi-purpose armored tractor or the BMP-3 infantry fighting vehicle, ensuring compatibility with mechanized units.[3] It accommodates 12 ready-to-fire 9M337 missiles housed in sealed transport-launch canisters arranged in two vertical banks of six, which protects them from environmental factors and allows rapid deployment.[3] Reloading the full complement requires approximately 12 minutes using standard equipment.[3] Mobility features include fire-on-the-move capability, permitting engagement of targets while the vehicle travels at speeds up to 60 km/h over rough terrain.[3] The system is operated by a two-person crew—a driver and a gunner—who manage detection, tracking, and launch from a protected cabin, supporting continuous operations in dynamic battlefield conditions.[3] The missile's two-stage propulsion further aids guidance stability during high-maneuver flight profiles.[11]Specifications and Performance
Key Technical Parameters
The 9M337 Sosna-R missile attains a maximum speed of Mach 2.6, equivalent to approximately 900 m/s, enabling rapid response to aerial threats.[1] This hyper-velocity performance supports its role in protecting military units from low-flying threats such as cruise missiles.[3] Its effective engagement range spans 1.3 to 10 km, with an altitude ceiling of 5 km (effective up to 3.5 km against certain targets).[1][2][9] The system operates across a broad environmental spectrum, including temperatures from -50°C to +50°C, and maintains functionality in day/night and adverse weather scenarios.[12] Resistance to electronic jamming is achieved through its multi-mode guidance, combining radio command in the initial phase with laser beam-riding for terminal control.[3] Key kinematic characteristics include a time-to-target of under 6 seconds for engagements within 5 km and approximately 11.5 seconds at the 8 km mark, reflecting efficient two-stage propulsion.[2] The missile's single-shot kill probability exceeds 0.8 against maneuvering aircraft, bolstered by a 7 kg warhead and high maneuverability up to 52g overload.[3][2][1]| Parameter | Value | Notes/Source |
|---|---|---|
| Maximum Speed | Mach 2.6 (900 m/s) | Average across sources; some cite up to 1,200 m/s.[1][3] |
| Engagement Range | 1.3–10 km | Effective against low-altitude targets; minimum 1.3 km.[1][2] |
| Maximum Altitude | 5 km (effective 3.5 km) | Ceiling for intercepts.[1][9] |
| Operational Temperature | -50°C to +50°C | System-wide tolerance based on platform.[12] |
| Time-to-Target (max range) | <6 s (short range); 11.5 s (8 km) | Kinematic flight duration.[2] |
| Single-Shot Kill Probability | >0.8 (up to 0.95) | Against maneuvering targets.[3] |