Worked as a research memeber in the project " LEOScan Optimizing SmallSat Constelltion for Enhanced STM and Space Debris Management in LEO "This is a collaborative international project platformed by Small Satellite Project group (SSPG) and the Space Safety &Sustainability Group (SSSPG)Constellation Design Team :Designed a SmallSat Constellation to monitor Space Debris in Low Earth Orbits (LEO) in the range of 600 to 1200 KMs. Also simulated the visibility results of the designed constillation and debris objects in FreeFlyer software to validate the results. Used novel techniques to improve the overall visibility of the debris objects while designing the satellite constellation. Interpreted the raw data from the FreeFlyer software using MATLAB scripting to calculate the overall constellation to debris visibility.

1.Supported the Vibration, Shock and Marine Vibrations for various products and also preparing the test setups.2. Understood the thermal testing process for electronic components along with physical data collection and its use for validation for thermal simulation results.3. Rendered models in Keyshort software and applied Artwork for the 3D models of the products.5. Conducted literature survey to create thermal network models for analytical calculations .6. Created an automated analytical approach that uses MATLAB to calculate temperatures of components before simulations.7. Created 3D models to perform ICEPAK simulation using PTC Creo.8. Performed Thermal Analysis on 3D models in ICEPAK to obtain results for the components.9. Took various trainings on PTC Creo, Matlab, Icepak and Ansys Workbench in the internship period.

STAR VTIP is a internship and training program that teaches the fundamentals of Spacecraft Dynamics and Orbital Mechanics and also provides hands on exercise to test and apply the acquired skills. A Lunar mission was designed in 3 phases to get a hands on from the theory learnt.PHASE 1:To calculate the delta-v required for the rocket to leave the Earth's Atmosphere and put the spacecraft into the Orbit considering forces on the rocket like Thrust, Weight and Drag.PHASE 2:To calculate the delta-v and the fuel required to perform a 3 orbit raising maneuvers and also to attain required velocity for Trans Lunar Injection and simulate the same in GMAT SoftwarePHASE 3:To design a trajectory for the landing of the lunar lander safely on the lunar surface

Worked on the project under the guidence of Shri.Vinod G.M (Scientist F) GTRE DRDO,along with other 3 members who are from the same university inorder to fulfill the academic requirements of the university for project completion