Search...
UUAVSale

WS-1B Multiple-Launch Rocket System

SKU: MD-P00774·UAV Platforms·Made to Order

WS-1B Multiple-Launch Rocket System
WS-1B Multiple-Launch Rocket System

Overview

WS-1 rocket launcher is an advanced long-range multi-tube uncontrolled rocket weapon system, which has the main characteristics of long range, high precision, good maneuverability, fast response, easy operation and maintenance, good safety and high reliability. The rocket is equipped with a multi-purpose warhead to strike at the enemy's deep surface targets. The WS-1B rocket launcher is an improved version of the original rocket launcher with a range of 180 kilometers. It has a diameter of 406 mm, a maximum range of 360 kilometers, and a killing radius of more than 450 meters. The weight of the warhead is 150 meters. Kilogram. Relevant experts pointed out that this is China s rocket launcher with the largest caliber and the longest range in the world. 1. Military bases, airports, ports, assembled fleets, important transportation hubs, military industrial bases 2. Political and economic center 3. Armored groups, artillery and missile launch positions, ground radar stations and their command and control centers 4. Other important military targets Tactical technical performance System response time: 20 minutes Launch method: Vehicle-mounted oblique launch (single shot or salvo) Engine: solid rocket motor Maximum flight speed: M=4.2 Projectile length: 4737mm Armor-piercing and anti-personnel dual-purpose submunition warhead Combined Effect Submunition Warhead kill deflagration warhead

Technical specification

Specifications. Key specifications: System response time 20 minutes, Launch method Vehicle-mounted oblique launch (single shot or salvo), Engine solid rocket motor, Maximum range 100 km, Minimum range 40 km, Shooting Intensity 1.0%, Maximum flight speed M=4.2, Projectile length 4737mm, Bullet diameter 302mm, Take-off mass 524 kg, Warhead mass 150 kg.

Technical specification — 1 groups
Key specifications: System response time 20 minutes, Launch method Vehicle-mounted oblique launch (single shot or salvo), Engine solid rocket motor, Maximum range 100 km, Minimum range 40 km, Shooting Intensity 1.0%, Maximum flight speed M=4.2, Projectile length 4737mm, Bullet diameter 302mm, Take-off mass 524 kg, Warhead mass 150 kg.

Technical specifications

Specifications

System response time
20 minutes
Launch method
Vehicle-mounted oblique launch (single shot or salvo)
Engine
solid rocket motor
Maximum range
100 km
Minimum range
40 km
Shooting Intensity
1.0%
Maximum flight speed
M=4.2
Projectile length
4737mm
Bullet diameter
302mm
Take-off mass
524 kg
Warhead mass
150 kg

Documents