Missile Hwasong-15

Description

The Hwasong-15 is a North Korean intercontinental ballistic missile developed as a successor to the Hwasong-14. Its development followed the cancellation of the Hwasong-13 project and an early 2017 announcement regarding the final stages of long-range missile testing. The system was first test-fired on November 28, 2017.

The missile utilizes a two-stage liquid propulsion system. The first stage incorporates the Paektusan engine, which consists of two combustors fed by a common turbopump using N2O4 and UDMH propellants. This stage employs a gimbaled two-chambered main engine system, a departure from earlier designs that used fixed chambers and vernier thrusters. The second-stage engine underwent independent testing in June 2017. The re-entry vehicle features a blunt nose cone designed to accommodate larger diameter nuclear warheads while reducing structural stress and thermal loading during atmospheric re-entry. Analysis indicates the payload section may support multiple warheads or decoys. A modified variant features an elongated shroud, a shortened first stage, and a potential third stage.

The Korean People's Army Strategic Force is the primary operator of the system. The missile is transported via a nine-axle transporter erector launcher, though flight tests have been conducted from fixed launch pads. The Hwasong-15 has appeared in military parades in 2018, 2020, and 2022. Following its initial 2017 test, a second flight was conducted on February 18, 2023, by the 1st Red Flag Hero Company. This launch was executed under a sudden order issued the same morning. A November 2022 test of a modified variant resulted in a flight failure following second-stage separation. There is no record of combat use.

Summary

CategoryBallistic Missiles
Sub-typeIntercontinental Ballistic Missile
Origin country 🇰🇵 North Korea
ManufacturerNorth Korea
StatusIn service
Year of service2017

Technical specifications

WarheadNuclear weapon
Diameter2,400 mm (94.5 in)
Length22,500 mm (885.8 in)
Flight altitude5,768,500 m (18,925,526 ft)
Weight72,000 kg (158,733 lb)
Range 13,000 km (8,078 mi)
Max. speed18,522 km/h (Mach 18.5)
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