Authoritative Insights by Dr. S. Unnikrishnan Nair (Former Director, VSSC & HSFC)
- Reentry Deceleration Physics: Any spacecraft re-entering Earth's atmosphere loses the bulk of its kinetic energy through atmospheric drag. However, as the Gaganyaan crew module descends into the lower atmosphere at ~170 m/s, specialized parachute systems must dissipate residual velocity to achieve a gentle touchdown of < 8.5 m/s.
- Multi-Staging Architecture: Under the Gaganyaan Crew Module Parachute Deceleration System ADRDE and Atmospheric Reentry Engineering, deploying a full-sized canopy instantly at high dynamic pressure would shred the fabric or induce fatal G-forces on astronauts. Staged deployment progressively increases canopy diameter to keep deceleration loads tolerable.
- Three Chute Types: The system incorporates: Pilot chutes (mini-chutes pulling out larger assemblies), Drogue chutes (conical chutes to stabilise aerodynamic attitude and drop speed), and Main chutes (broad canopies for final descent).
- Wake Penetration Ejection: The blunt conical crew module generates a turbulent aerodynamic wake in its rear. Mortar-based pyrotechnic ejection imparts sufficient initial velocity to pierce this wake and deploy canopies in undisturbed airflow.
| Aerospace Polymer / Material | Sub-System Application | Engineering Property & Operational Function |
|---|---|---|
| Kevlar (Aramid Polymer) | High-load suspension lines, risers, and structural reinforcement tapes. | Exceptional tensile strength-to-weight ratio and minimal elongation under violent shock opening loads in Gaganyaan Crew Module Parachute Deceleration System ADRDE and Atmospheric Reentry Engineering. |
| Nomex (Flame-Resistant Meta-Aramid) | Heat-shielded skirt regions and mortar discharge zones. | Withstands hot mortar gas discharge, aerothermal plume heating, and frictional thermal spikes. |
| High-Tenacity Nylon | Canopy broadcloths and gores. | High elastic elongation absorbs initial dynamic opening shock; high compressibility allows ultra-dense vacuum packing in limited stowage volumes. |
Rail Track Rocket Sled (RTRS)
Conducted at Terminal Ballistic Research Lab (TBRL), Chandigarh, testing mortar ejection and canopy inflation at precise supersonic/transonic dynamic pressures under Gaganyaan Crew Module Parachute Deceleration System ADRDE and Atmospheric Reentry Engineering.
2-out-of-3 Main Chute Redundancy
Developed by ADRDE Agra (DRDO), if any single main parachute suffers an anomaly, the remaining two independent chutes ensure full crew survivability and safe splashdown.
Following ocean touchdown, pyrotechnic reefing line cutters instantly detach parachute risers to prevent surface wind drags or sea capsizing, validating Gaganyaan Crew Module Parachute Deceleration System ADRDE and Atmospheric Reentry Engineering.
1. The Aerial Delivery Research and Development Establishment (ADRDE), a premier laboratory of DRDO located in Agra, is the lead developer of the parachute deceleration system.
2. Drogue parachutes are deployed prior to main parachutes to stabilise the crew module and reduce high dynamic pressures during atmospheric descent.
3. In the Gaganyaan crew module, Nomex polymer is primarily utilized for canopy broadcloth due to its high elasticity, while Nylon is used exclusively for hot gas mortar blast shields.
Which of the statements given above is/are correct?
Correct Answer: A — 1 and 2 only
Statement 3 is incorrect because Nylon is used for the canopy broadcloth due to its high elasticity to absorb inflation shocks, whereas Nomex is flame-resistant and used in heat-exposed mortar discharge zones. Statements 1 and 2 are correct.
1. Gaganyaan is India's maiden human spaceflight mission aiming to demonstrate human spaceflight capability to Low Earth Orbit (LEO).
2. The Human Space Flight Centre (HSFC) under ISRO is responsible for the implementation of the Gaganyaan project.
Which of the statements given above is/are correct?
A) 1 only
B) 2 only
C) Both 1 and 2
D) Neither 1 nor 2
Correct Answer: C — Both 1 and 2
Both statements are correct. Gaganyaan aims to demonstrate indigenous human spaceflight to a 400 km LEO orbit for up to 3 days, orchestrated by ISRO's HSFC in Bengaluru.
UPSC CSE Mains 2022 — GS Paper III (Official Question)
Mains Model Blueprint (15 Marks | 250 Words)
Key Answer Framework
- Introduction: Define atmospheric reentry dynamics and contextualise the Gaganyaan Crew Module Parachute Deceleration System ADRDE and Atmospheric Reentry Engineering.
- Aerodynamic & Thermal Challenges: Dissipating hypersonic kinetic energy, managing plasma heat shields, and overcoming the turbulent wake of blunt re-entry capsules.
- Multi-Staged Deceleration Architecture: Sequential deployment of mortar-fired drogue chutes for attitude stabilization, followed by pilot and cluster main parachutes.
- Material Innovations & Testing: Role of Kevlar, Nomex, and Nylon; ground qualification via Rail Track Rocket Sleds (RTRS) and integrated airdrop tests (IADT).