• Developed preliminary concept of operations for an on-orbit refuelling mission of a spacecraft.• Computed fuel expenditure for the rendezvous and proximity operations in Python and AGI STK, along with sensitivity analyses. • Defined safety requirements for the on-orbit refuelling vehicle.

• Intern at the Aeronautical Development Establishment - DRDO• Bachelor thesis, titled: "Numerical and Experimental Investigation of Cavity Flow Field in the Presence of Store".• Performed numerical analysis for a store within a cavity in ANSYS Fluent.• Post-processed the results in Origin Pro. • Designed a test model for the wind tunnel validation experiment using SolidWorks ensuring its manufacturability.

• Headed and managed the thermal subsystem consisting of six members.• Established the requirements, risk management plan, and work breakdown structure for the subsystem• Coordinated closely with other subsystems, external stakeholders and manufacturers. • Responsible for interviewing potential candidates and subsequently training the new members.

• Involved in selecting the solid rocket motor for our first rocket.• Worked on the integration of the thermal and pressure sensors with the static firetest model.

• Responsible for promoting Team Antariksh and its projects at events and all public platforms.• Created social media content using Adobe Photoshop and Premiere Pro.• Designed promotional banners, business cards for team leads, team pamphlets, team t-shirts, and team handbook.• Led and supervised a group of seven members working on social media content and team website.• Acted as designated photographer for the team at events.