S-24 rocket: Difference between revisions
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The S-24 is {{convert|2.33|m|ftin}} long, with a launch weight of {{convert|235|kg|lb|abbr=on|sigfig=2}}. It has a {{convert|123|kg|lb|abbr=on|adj=on}} blast-[[fragmentation (weaponry)|fragmentation]] [[warhead]]. Its range is about {{convert|2|-|3|km|mi}}. The S-24 is carried individually on weapon [[hardpoints]], rather than in pods. | The S-24 is {{convert|2.33|m|ftin}} long, with a launch weight of {{convert|235|kg|lb|abbr=on|sigfig=2}}. It has a {{convert|123|kg|lb|abbr=on|adj=on}} blast-[[fragmentation (weaponry)|fragmentation]] [[warhead]]. Its range is about {{convert|2|-|3|km|mi}}. The S-24 is carried individually on weapon [[hardpoints]], rather than in pods. | ||
Proximity fuze RV-24 is also available, in which the warhead detonate 3 meters above ground, creating 300–400 m radius of fragmentation casualty zone.<ref name=airwar.ru /> The body is mesh-texture shape-hardened by electric treatment and creates 4000 fragments that can penetrate up to 30 millimeters of armor, though some sources dispute this and give a figure of 25 millimeters. | [[Proximity fuze]] RV-24 for [[airburst]] is also available, in which the warhead detonate 3 meters above ground, creating 300–400 m radius of fragmentation casualty zone.<ref name=airwar.ru /> The body is mesh-texture shape-hardened by electric treatment and creates 4000 fragments that can penetrate up to 30 millimeters of armor, though some sources dispute this and give a figure of 25 millimeters. | ||
The rocket is also license produced in [[Iran]] under the name of Shafaq.<ref>{{cite web |url=http://www.iranwatch.org/suspect/records/aerospace-industries-organization-%28aio%29.html |title=Iranian Entity: Aerospace Industries Organization (AIO)|website=www.iranwatch.org |archive-url=https://web.archive.org/web/20120107030715/http://www.iranwatch.org/suspect/records/aerospace-industries-organization-%28aio%29.html |archive-date=January 7, 2012}}</ref><ref>{{usurped|1=[https://archive.today/20120905180352/http://www.modlex.ir/cgi-bin/store.pl/page=product.html/pid=MXF05-000310 Article title]}} </ref> | The rocket is also license produced in [[Iran]] under the name of Shafaq.<ref>{{cite web |url=http://www.iranwatch.org/suspect/records/aerospace-industries-organization-%28aio%29.html |title=Iranian Entity: Aerospace Industries Organization (AIO)|website=www.iranwatch.org |archive-url=https://web.archive.org/web/20120107030715/http://www.iranwatch.org/suspect/records/aerospace-industries-organization-%28aio%29.html |archive-date=January 7, 2012}}</ref><ref>{{usurped|1=[https://archive.today/20120905180352/http://www.modlex.ir/cgi-bin/store.pl/page=product.html/pid=MXF05-000310 Article title]}} </ref> | ||
Latest revision as of 17:24, 8 August 2025
The S-24 is a rocket weapon designed and used by the Soviet Air Force. It remains in use by the Russian Aerospace Forces, Ukrainian Air Force and many export countries. The name is based on the diameter of the rocket, Script error: No such module "convert"..
The Soviet Union was an enthusiastic user of rocket weapons, employing them as early as the 1930s. The S-24/S-24B is a very large, powerful unguided weapon and one of a handful of successors to the earlier World War II-era BETAB-750DS rockets.[1]
The S-24B differs from the S-24 in that it uses BN-K low smoke motor powder for a low-smoke flight.[2][3][4]
The S-24 is Script error: No such module "convert". long, with a launch weight of Script error: No such module "convert".. It has a Script error: No such module "convert". blast-fragmentation warhead. Its range is about Script error: No such module "convert".. The S-24 is carried individually on weapon hardpoints, rather than in pods.
Proximity fuze RV-24 for airburst is also available, in which the warhead detonate 3 meters above ground, creating 300–400 m radius of fragmentation casualty zone.[3] The body is mesh-texture shape-hardened by electric treatment and creates 4000 fragments that can penetrate up to 30 millimeters of armor, though some sources dispute this and give a figure of 25 millimeters.
The rocket is also license produced in Iran under the name of Shafaq.[5][6]
See also
References
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