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Science & Technology July 05, 2026 4 min read Daily brief · #2 of 2

Gaganyaan mission: Isro's parachute test vehicle clears first ground test

ISRO successfully conducted the first static ground test of the solid motor for SOLVE (Sub-Orbital Launch Vehicle for Experiments), a dedicated test platform...


What Happened

  • ISRO successfully conducted the first static ground test of the solid motor for SOLVE (Sub-Orbital Launch Vehicle for Experiments), a dedicated test platform developed for validating the Gaganyaan crew module's parachute recovery system.
  • The solid motor was fired at the Static Test Facility at the Satish Dhawan Space Centre (SDSC), Sriharikota, in a test lasting approximately ten hours.
  • SOLVE was developed by modifying the solid-fuel strap-on motors used in ISRO's Polar Satellite Launch Vehicle (PSLV), with key changes including a slow-burning propellant formulation and a straight nozzle with secondary injection thrust vector control.
  • The vehicle is designed to carry a representative crew module to altitudes of 10–17 km, after which a 10-parachute deployment sequence will be triggered to test descent and splashdown recovery.
  • This ground test precedes integrated air drop tests and eventual full-scale parachute validation flights, which are critical before the first uncrewed Gaganyaan mission (G1) planned for 2026.

Static Topic Bridges

Gaganyaan — India's Human Spaceflight Programme

Gaganyaan is ISRO's flagship programme to place a crew of three Indian astronauts into Low Earth Orbit (LEO) at an altitude of ~400 km for a 3-day mission, then return them safely. Approved by the Union Cabinet in December 2018 with an initial budget of ₹10,000 crore, the budget was subsequently enhanced to ₹20,000 crore (Cabinet approval, September 2024). If successful, India will become the fourth country to independently launch humans into orbit, after the United States, Russia, and China.

  • Launch vehicle: Human Rated LVM3 (LVM3-H), a crewed variant of Launch Vehicle Mark-III
  • Crew module re-entry and parachute recovery is designed to end with a sea splashdown in the Bay of Bengal
  • Four IAF pilots selected as Gaganauts: Prasanth Balakrishnan Nair, Ajit Krishnan, Angad Pratap, and Shubhanshu Shukla
  • Flight sequence: G1 (uncrewed, with Vyommitra humanoid robot) → G2 → G3 → H1 (first crewed flight, targeted Q1 2027)
  • ISRO completed over 8,000 cumulative ground tests across subsystems by 2026

Connection to this news: SOLVE is a purpose-built test rocket to validate the 10-parachute recovery system that will bring the Gaganyaan crew module safely back to Earth; this ground test is the foundational step before integrated in-flight parachute trials.

Parachute Recovery Systems in Crewed Spaceflight

A parachute recovery system (also called a recovery parachute system or RPS) is the final deceleration mechanism used to bring a crewed capsule from high-speed atmospheric re-entry to a safe touchdown or splashdown speed. Systems typically use a staged deployment: drogue chutes deploy first at higher altitudes to stabilize and slow the capsule, followed by larger main parachutes that further reduce terminal velocity to safe levels (typically 5–10 m/s at touchdown).

  • Gaganyaan's 10-parachute system includes: 2 apex cover separation parachutes (Ø 2.5 m), 2 drogue parachutes (Ø 5.8 m), 3 pilot parachutes (Ø 3.4 m), and 3 main parachutes (Ø 25 m)
  • ISRO also conducted Integrated Air Drop Tests (IADT) using IAF Chinook helicopters dropping a 4.8-tonne crew module mock-up from ~3 km over the Bay of Bengal — the second IADT was completed on 10 April 2026
  • The parachute system must handle both nominal re-entry and abort scenarios (e.g., Crew Escape System activation at low altitude)

Connection to this news: The SOLVE solid motor test is the precursor to high-altitude parachute deployment tests that cannot be validated cheaply with a full LVM3; SOLVE provides a cost-effective, dedicated test environment.

Sub-Orbital Launch Vehicles — Role in Space Technology Development

A sub-orbital vehicle reaches space or the upper atmosphere but does not achieve the orbital velocity (approximately 7.9 km/s) needed to circle Earth. Such vehicles are used for microgravity experiments, atmospheric research, and, critically, for testing re-entry and recovery technologies at realistic altitudes and velocities without the cost of an orbital launch. ISRO previously used a Test Vehicle (TV-D1) to test the Crew Escape System in October 2023; SOLVE extends this test-flight philosophy to parachute systems.

  • SOLVE is derived from PSLV strap-on solid motors (PS2S / PSOM class), modified with a slow-burn propellant and secondary injection thrust vector control
  • Target test altitude: 10–17 km — sufficient to replicate drogue and main chute deployment conditions
  • The approach mirrors NASA's use of the Pad Abort Test and Liberty Bell abort test vehicles, and Russia's use of specialized recovery test rockets for Soyuz

Connection to this news: By successfully firing SOLVE's solid motor at Sriharikota, ISRO validated the propulsion element of this dedicated test platform, clearing the way for full-scale integrated parachute drop tests.

Key Facts & Data

  • SOLVE full form: Sub-Orbital Launch Vehicle for Experiments
  • Gaganyaan budget: ₹10,000 crore (2018 approval); enhanced to ₹20,000 crore (September 2024 Cabinet approval)
  • Target orbit: ~400 km LEO; mission duration: 3 days
  • Number of parachutes in Gaganyaan recovery system: 10 (staged deployment)
  • Main parachutes diameter: 25 m each (3 units)
  • SOLVE test altitude range: 10–17 km
  • Test facility: Static Test Facility, Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh
  • India would be the 4th country to independently achieve human orbital spaceflight (after USA, Russia, China)
  • First crewed mission (H1) targeted: Q1 2027
  • Four Gaganauts selected, all IAF pilots
  • Second Integrated Air Drop Test completed: 10 April 2026
On this page
  1. What Happened
  2. Static Topic Bridges
  3. Gaganyaan — India's Human Spaceflight Programme
  4. Parachute Recovery Systems in Crewed Spaceflight
  5. Sub-Orbital Launch Vehicles — Role in Space Technology Development
  6. Key Facts & Data
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