ISRO Tests Solid Motor Sub-Orbital Launch Vehicle (SOLVE)

ISRO Tests Solid Motor Sub-Orbital Launch Vehicle (SOLVE)

#GS-3 #Science & Technology #Space #Current Events #National #ISRO #SOLVE #Gaganyaan Mission

Key takeaways

  • ISRO successfully performed the first ground test of the Sub-Orbital Launch Vehicle for Experiments (SOLVE) at Sriharikota.
  • The vehicle carries cargo up to an altitude between 10 km and 17 km to test re-entry conditions.
  • It relies on a modified PSLV Strap-on Motor (PSOM) and Secondary Injection Thrust Vector Control (SITVC) for stable flight.
  • The primary goal is testing the 10-parachute recovery sequence designed for the Gaganyaan crew module.

Why in News

  • The ISRO completed the first ground test of its Sub-Orbital Launch Vehicle for Experiments (SOLVE) engine at Sriharikota.

Overview of SOLVE

  • Engineers designed SOLVE as a solid propellant test rocket to evaluate equipment at high altitudes without using full orbital vehicles.
  • The Indian Space Research Organisation (ISRO) leads the design and operation of this dedicated testing platform.

Key Objectives

  • The platform conducts Integrated Parachute Tests (IPT) to check the safe landing system of the Gaganyaan crew capsule.
  • It carries experimental instruments to high altitudes so teams can study how hardware responds to actual flight conditions.

How SOLVE Works

  • A modified solid fuel burns slowly inside the motor to ensure a smooth ascent instead of sharp acceleration.
  • The launch vehicle transports the Gaganyaan test capsule up to an altitude between 10 km and 17 km.
  • At peak height, the vehicle releases the capsule to expose it directly to heavy atmospheric friction and forces.
  • After separation, an automated system opens 10 distinct parachutes sequentially to slow the module before landing in the ocean.

Key Engineering Features

  • ISRO built SOLVE using a modified PSLV Strap-on Motor (PSOM) to lower development costs.
  • Engineers formulated a slow-burning solid propellant to deliver steady thrust throughout the test phase.
  • A straight nozzle paired with Secondary Injection Thrust Vector Control (SITVC) guides the vehicle along its path.
  • The structure recreates realistic aerodynamic speeds and pressures to mirror actual re-entry profiles.

Uses and Applications

  • The system verifies the 10-parachute recovery sequence required to return Indian astronauts safely from space.
  • It lowers testing costs by avoiding the expense of full-scale multi-stage rocket launches.
  • The rocket aids domestic space research in hypersonic flight, atmospheric science, and microgravity experiments.