Scramjet Engine

Scramjet Engine

  • The Scramjet engine designed by ISRO uses Hydrogen as fuel and the Oxygen from the atmospheric air as the oxidiser.
  • The first experimental mission of ISRO’s Scramjet Engine towards the realisation of an Air Breathing Propulsion System was successfully conducted on August 28, 2016

  • A ramjet is a type of air-breathing jet engine that operates on the principle of the ram effect.
  • It consists of an inlet, a combustion chamber, and a nozzle.
  • The engine relies on the forward motion of the aircraft to compress incoming air before combustion.
  • Ramjets are most efficient at high speeds, typically above Mach 2 (twice the speed of sound).
  • They are not self-starting and require an initial acceleration to achieve the necessary air compression for combustion.
  • A scramjet, or Supersonic Combustion Ramjet, is an advanced version of the ramjet.
  • It operates on the same basic principles as a ramjet but can efficiently operate at even higher speeds.

Human Rated Launch Vehicle (HRLV)

  • The primary mandate of HSFC is to spearhead ISRO’s Gaganyaan programme
  • LVM3 rocket – The well proven and reliable heavy lift launcher of ISRO, is identified as the launch vehicle for Gaganyaan mission.
  • It consists of solid stage, liquid stage and cryogenic stage. All systems in LVM3 launch vehicle are re-configured to meet human rating requirements and christened Human Rated LVM3.
  • HLVM3 will be capable of launching the Orbital Module to an intended Low Earth Orbit of 400 km.
  • HLVM3 consists of Crew Escape System (CES) powered by a set of quick acting, high burn rate solid motors which ensures that Crew Module along with crew is taken to a safe distance in case of any emergency either at launch pad or during ascent phase.
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