BrahMos-II Hypersonic Missile

From Astra Kosh, the AlphaDefense encyclopedia · Category: Strategic Systems

BrahMos-II (also BrahMos-2) is a hypersonic scramjet-propelled cruise missile under joint development by India’s DRDO and Russia’s NPO Mashinostroyenia (via the BrahMos Aerospace joint venture), conceived as a hypersonic-class successor to the supersonic BrahMos, aimed at delivering both dramatically reduced enemy reaction time and improved penetration against modern air-defence systems.[1]

Design

BrahMos-II is designed around scramjet (supersonic-combustion ramjet) air-breathing propulsion for its cruise phase, targeting a maximum speed of approximately Mach 8 — placing it firmly in the hypersonic regime — and a range of around 1,500 km. Scramjet propulsion at this speed regime represents one of the most demanding areas of missile propulsion engineering, requiring materials and combustion-control technology that only a handful of countries have successfully demonstrated.[1]

Status and Significance

As a joint India-Russia programme building on the mature BrahMos partnership, BrahMos-II represents India’s most ambitious hypersonic cruise-missile effort, complementing DRDO’s separate indigenous hypersonic glide-vehicle and boost-glide programmes. Its long and technically demanding development timeline reflects the broader global difficulty of fielding operational scramjet-powered hypersonic cruise weapons.[2]

Specifications

Type Hypersonic, scramjet-propelled cruise missile
Developers DRDO (India) and NPO Mashinostroyenia (Russia), via BrahMos Aerospace
Propulsion Scramjet (air-breathing, supersonic combustion)
Target speed ~Mach 8
Target range ~1,500 km
Predecessor BrahMos (supersonic cruise missile)
Status Under development

Sources

  1. Wikipedia, “BrahMos-II.”
  2. Missile Defense Advocacy Alliance, “BrahMos II.”