The S-400 Triumf (Russian: C-400 «триумф», Triumph; NATO reporting name: SA-21 Growler), already known as S-300PMU-3, is a hostile to flying machine weapon framework created by Russia's Almaz Central Design Bureau in the 1990s as an update of the S-300 family. It has been in administration with the Russian Armed Forces since 2007.
The S-400 utilizations three distinct rockets to cover its whole execution envelope. These are the greatly long range 40N6, long range 48N6 and medium extent 9M96 rocket.
The improvement of the S-400 framework started in the late 1990s. The framework was formally reported by the Russian Air Force in January 1999. On 12 February 1999, the principal tests were performed at Kapustin Yar in Astrakhan which were accounted for fruitful. As an aftereffect of this, the S-400 was planned for organization in the Russian armed force in 2001.
In 2003 it first got to be obvious that the framework was not prepared for organization, and in August two high-positioning military authorities communicated worries that the S-400 was being tried utilizing "out of date" interceptors from the S-300P and inferred that it was not prepared for generation.
The finish of the venture was declared in February 2004. In April, a ballistic rocket was captured in a test of the redesigned 48N6DM interceptor rocket. Authoritatively acknowledged for administration in 2007.
Structure
30K6E organization framework: oversees 8 divisions (units)
55K6E order and control focus in view of Ural-532301.
91N6E Panoramic radar recognition framework (scope of 600 km) with insurance against sticking. Mounted on a MZKT-7930. 300 targets. Decimetric band (S).
6 units of 98ZH6E Surface-to-air rocket frameworks comprising of (a free battle framework for self-governing operation): Each legion can hit close to 6 focuses on their own.+2 another regiments in the event that they are inside reach 40 km.
92N6(or 2)E Multi-practical radar (scope of 400 km). 100 targets.
5P85TE2 launchers and/or 5P85SE2 on the trailer (up to 12 launchers).
Surface-to-air rockets permitted by Russian Presidential announcement: 48N6E, 48N6E2, 48N6E3, 48N6DM, 9M96E, 9M96E2 and the ultra - long range 40N6E.
The S-400 uses an active electronically scanned array (official government explanation)
Conceivable components of the S-400 (98ZH6E): 15I6ME – 98ZH6E with scope of 30/60/90 km working outside 30K6E scope. 96L6E – general complex (all capacities), identification scope of 300 km. 40B6M – lodging for 92N6E or 96L6E sort radar. Against – stealth: Protivnik-GE, Gamma-DE. Orion detached sensor (locator) for target assignment reporting in real time barrier framework (facilitates 1 out of 3), Avtobaza-M uninvolved sensor (locator) for target assignment broadcasting live safeguard framework (organizes 2 out of 3) and Orion+ Avtobaza=the careful area. 1RL220BE characterized data (or obsolete), more seasoned variants (probably) were utilized for obstruction/against sticking (inside/inside aloof sensor (locator)). It is Possible to use the S-200D "Dubna" (SA-5c) rockets (400 km), and in addition different radar frameworks of the S-300 (Air Defense variants (P family)) without the utilization of extra summon and control focuses. The S-300 (SA-20A/SA-20B) sort rockets can likewise be controlled and guided . A-50/A-50U flying machine early cautioning, summon and control exchange target assignment
The 30к6е control framework can be incorporated with the:
S-400 Triumph 98ZH6E framework;
S-300PMU2 (through the 83м6е2 control framework);
S-300PMU1 (through the 83м6е control framework);
Tor-M1 through the Ranzhir-M battery order post;
Pantsir-S1 through the lead battery vehicle;
Triumf kets – when completing extra errands utilizing the 30K6E organization framework; gathering of the course data from an extra incorporated 92н6е radar framework;
Radar sort 96L6E/30K6E organization framework, Protivnik-GE, Gamma-DE. Discretionary incorporation with the 92H6E radar framework empowers correspondence between every battery with:
Baikal-E senior charge posts and other comparable sorts;
adjacent 30к6е, 83м6е, and 83м6е2 organization frameworks ;
Polyana-D4м1 charge post;
Charge post for Russian contender flying machine.
For fare to remote clients, with the motivation behind coordinating existing client air resistance frameworks, extra work on change of the 30K6E organization framework for data innovation matching with hostile to kets is in advancement.
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