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Science & Technology July 05, 2026 4 min read Daily brief · #1 of 6

Gaganyaan mission: ISRO successfully conducts first SOLVE ground test

ISRO successfully conducted the first static ground test of the solid rocket motor for its Sub-Orbital Launch Vehicle for Experiments (SOLVE) at the Static T...


What Happened

  • ISRO successfully conducted the first static ground test of the solid rocket motor for its Sub-Orbital Launch Vehicle for Experiments (SOLVE) at the Static Test Facility, Satish Dhawan Space Centre (SDSC-SHAR), Sriharikota, on July 3, 2026.
  • SOLVE is a dedicated test platform being developed to carry out Integrated Parachute Tests (IPTs) for validating the parachute-based deceleration system of the Gaganyaan Crew Module under a range of descent conditions.
  • The solid motor powering SOLVE is derived from the PSLV strap-on motor, with several modifications introduced to meet human-spaceflight safety standards.
  • During future experimental flights, SOLVE will carry the Crew Module to an altitude of 10–17 km, after which the module will separate and deploy a sequence of parachutes to execute a controlled descent and splashdown.
  • This ground test confirms motor performance before SOLVE proceeds to integrated air-drop and sub-orbital flight tests.

Static Topic Bridges

Gaganyaan Programme

Gaganyaan is India's first human spaceflight programme, formally announced in August 2018. Its objective is to demonstrate an end-to-end capability for crewed low Earth orbit (LEO) missions, carrying a crew of two or three to an altitude of approximately 400 km for up to seven days. The launch vehicle is the Human-Rated LVM3 (HLVM3), a three-stage rocket standing 53 m tall with a lift-off mass of 640 tonnes. The programme follows a phased approach: uncrewed demonstration flights (Gaganyaan-1, Gaganyaan-2, Gaganyaan-3) precede the first crewed mission, currently expected no earlier than 2027.

  • Launch vehicle: HLVM3 (modified LVM3 / GSLV Mk III), capable of lifting 4,000 kg to geosynchronous transfer orbit
  • Crew module designed for two or three astronauts; capsule mass approximately 5.3 tonnes
  • Mission altitude: ~400 km LEO; maximum mission duration: seven days
  • Splashdown recovery zone: Bay of Bengal

Connection to this news: SOLVE validates the parachute deceleration system, a mission-critical subsystem for safe crew module recovery — without successful parachute qualification, the crewed Gaganyaan missions cannot proceed.

Parachute-Based Deceleration System

The Gaganyaan Crew Module employs a staged parachute deployment sequence to reduce re-entry descent velocity from approximately 700 km/h to around 30 km/h at splashdown. The system uses ten parachutes in sequence: two Apex Cover Separation (ACS) parachutes, two Drogue parachutes, three Pilot parachutes, and three Main parachutes. The parachutes are jointly developed by ISRO and the Defence Research and Development Organisation (DRDO). The SOLVE platform enables ground-based and sub-orbital testing of this system to qualify it for actual crewed missions.

  • Two Drogue parachutes stabilise the module after ACS deployment
  • Three Main parachutes provide the terminal deceleration for splashdown
  • Target touchdown velocity: approximately 30 km/h (from ~700 km/h re-entry speed)
  • DRDO contributes parachute canopies; ISRO integrates the system into the Crew Module

Connection to this news: The SOLVE ground test validates the solid motor that will carry the Crew Module to the required altitude for integrated parachute tests, making it a precursor to system-level qualification.

Crew Escape System (CES) and Human-Rating of Launch Vehicles

The Crew Escape System is a rapid-abort safety mechanism positioned at the forward end of HLVM3. In the event of a launch anomaly, high-burn solid motors pull the Crew Module away from the rocket within seconds, allowing safe parachute-assisted descent. India's CES uses a "puller-type" design (as opposed to SpaceX's "pusher-type"). The Integrated Vehicle Health Management (IVHM) system monitors parameters in real time and triggers the CES automatically if a critical anomaly is detected. ISRO tested the CES in 2023 (TV-D1 mission) at Sriharikota.

  • CES tested in TV-D1 abort demonstration mission (October 2023)
  • Crew module descended safely into Bay of Bengal using parachutes during TV-D1
  • Human-rating requires rigorous qualification of all safety-critical subsystems
  • India joins the US, Russia, and China in possessing human-rated launch abort capability

Connection to this news: SOLVE-based parachute testing complements the CES qualification programme; together they form the complete crew safety and recovery architecture for Gaganyaan.

PSLV and Solid Propulsion Heritage

The Polar Satellite Launch Vehicle (PSLV) has been ISRO's most reliable workhorse since its first successful flight in 1994. Its first stage (PS1) and strap-on boosters use solid propellant motors. ISRO's expertise in solid propulsion — developed through PSLV and earlier SLV/ASLV programmes — enables the reuse and adaptation of proven motor designs for new applications such as SOLVE. This design heritage approach reduces development risk and cost.

  • PSLV strap-on (PSOM): hydroxyl-terminated polybutadiene (HTPB)-based solid motor
  • PSLV has achieved over 50 consecutive successful missions
  • SDSC-SHAR, Sriharikota is the primary Indian spaceport and hosts the Static Test Facility used for SOLVE

Connection to this news: SOLVE's solid motor is adapted from the PSLV strap-on, demonstrating ISRO's strategy of leveraging proven solid propulsion heritage for new mission-specific test vehicles.

Key Facts & Data

  • SOLVE full form: Sub-Orbital Launch Vehicle for Experiments
  • Test location: Static Test Facility, Satish Dhawan Space Centre (SDSC-SHAR), Sriharikota
  • Ground test date: July 3, 2026
  • Gaganyaan target altitude: ~400 km LEO
  • Crew module mass: ~5.3 tonnes; crew capacity: 2–3 astronauts
  • Parachute sequence: 10 parachutes total (2 ACS + 2 Drogue + 3 Pilot + 3 Main)
  • Descent velocity reduction: ~700 km/h (re-entry) to ~30 km/h (splashdown)
  • SOLVE flight altitude for parachute tests: 10–17 km
  • HLVM3 height: 53 m; lift-off mass: 640 tonnes
  • Gaganyaan crewed flight target: no earlier than 2027
  • TV-D1 (Crew Escape System test): successfully conducted October 2023
On this page
  1. What Happened
  2. Static Topic Bridges
  3. Gaganyaan Programme
  4. Parachute-Based Deceleration System
  5. Crew Escape System (CES) and Human-Rating of Launch Vehicles
  6. PSLV and Solid Propulsion Heritage
  7. Key Facts & Data
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