Parth Jain
Aerospace engineer focused on the complete lifecycle of flight-ready hardware. My experience spans structural design, thermal analysis, and systems engineering across both the space and defence sectors. From leading the team that launched India's first student-built supersonic rocket to modelling aerobraking strategies for ISRO, I specialise in translating complex simulations into physical systems that thrive in extreme environments.
Project
AgniAstra
India's first student-built supersonic sounding rocket. Led a 54-member team as Project Manager and Structural Design Engineer at Spaceport America Cup 2024.
MIRA Space Telescope
Miniaturised optical space telescope by Eon Space Labs. Led mechanical systems design, achieving a 16% mass reduction. Oversaw AIT and integration with the MOI-1 satellite for PSLV-C62.
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Venus Aerobraking Control Strategies
High-fidelity aerothermal braking simulations for Venus atmospheric entry using SPARTA for rarefied gas dynamics. ISRO.
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Airbus Sloshing Rocket Workshop
Sloshing rocket designed for the EUROAVIA x Airbus competition. Structural design, CAD, fabrication, and testing of a liquid-payload rocket.
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NACDeC VII – Team FlightForge
2nd Place · 45 Teams Nationwide. Solar-powered UAV for Martian atmospheric research. Won ₹1,25,000.
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Project Altair
10K COTS rocket built for Spaceport America Cup 2023. Reached 10,331 ft with 0.51% apogee error.
View Project Details →Design Validation of Aluminium Sounding Rocket Fins Under Supersonic Flight Conditions
International Conference on Advances in Aerospace and Energy Systems (IAES 2026)
Accepted March 2026
Multiphysics validation of aluminium rocket fins for supersonic flight, combining CFD, fluid-structure interaction, and structural simulations. The optimized design balances drag, thermal resistance, and aeroelastic stability, demonstrating safe performance under peak flight conditions.
Predictive Thermal Control Strategies for Aerobraking: Peak Temperature Forecasting and Adaptive Maneuvers
28th National and 6th International ISHMT–ASTFE Heat and Mass Transfer Conference
Presented December 2025
Forecasting peak thermal loads during aerobraking and developing adaptive control strategies to ensure spacecraft survivability during atmospheric passes.
Published in the ISHMT Digital Library
Project AgniAstra - Technical Report, Spaceport America Cup 2024
Spaceport America Cup 2024 · 30K COTS · Manipal Academy of Higher Education
June 2024
30K COTS vehicle for Spaceport America Cup 2024 targeting 30,000 ft apogee. Carbon and glass fibre composite fuselage, Cesaroni Pro98 motor, dual-event parachute recovery, and a nosecone-housed CanSat payload with IR camera and onboard computer vision for real-time pose tracking.
Published on ResearchGate
Sounding Rocket Device with Fin and Motor Alignment Attachment
Application No. 202441075844
Attachment mechanism for precise fin and motor alignment in high-performance sounding rockets, enabling repeatable structural integrity under supersonic loads.
The problems that interest me most lie where physics becomes unforgiving and engineering must become precise.
High-speed aerodynamics, atmospheric entry, and spaceflight systems all operate in regimes where small design decisions carry enormous consequences. I want to work on vehicles that push into those regimes and build the engineering systems that allow them to operate safely, predictably, and repeatedly.
Leading mechanical systems design, structural analysis, and integration testing across all hardware products.
Developed aerobraking control strategies for upcoming interplanetary missions. Built a comprehensive simulation framework integrating DSMC aerothermal analysis, orbital mechanics, and thermal modelling.
