Naman Jain
Melbourne,FL
Summary
I’m an aerospace Engineer with an M.S. from Florida Institute of Technology, specializing in UAV systems, propulsion, and aerodynamic analysis. Skilled in designing VTOL UAVs, developing control algorithms (MPC), and performing CFD simulations. Proficient in ANSYS, MATLAB, and Simulink. Obsessive about advancing aerospace technologies through innovative design and systems.
Offering strong analytical skills and passion for technology, eager to learn and thrive in engineering environment. Brings solid understanding of engineering principles and ability to quickly learn industry-specific tools and methodologies. Ready to use and develop problem-solving and technical skills in Desired Position role.
Overview
3
3
years of professional experience
Work History
Engineer, Entry, Decent and Landing
NASA L'SPACE NPWEE
Remote
09.2024 - 12.2024
- Attended 16+ NASA-led sessions on proposal writing, failure analysis, and EDL systems.
- Defined technical goals for an EDL concept using risk-based design methodology.
- Proposed a novel EDL tech solution with integrated corrective action strategy.
- Conducted 5+ trade studies on Mars EDL systems aligned with NASA requirements.
- Evaluated mission risks and reliability using quantitative failure analysis tools.
Academic Intern
Gnat Aviation Design Development of VTOL UAV
Remote
10.2021 - 12.2021
- Ran a three-option turbo generator trade study and selected the 90 kW TG-R90 (1.4 kW kg⁻¹) as the optimum VTOL power source.
- Created charts for a 300 kg MTOW UAV (FoS 1.5) and specified 4× ERMAX 228 lift motors plus an ERMAX 208 pusher.
- Architected the hybrid-electric stack, selecting the ATL-794 fuel tank, Li-ion battery, R15VOL regulator, PM100 inverter and AP10.1 flight controller on a 90 kW DC bus.
- Derived CD₀ = 0.025 and induced-drag constants via component build-up and lifting-line theory, achieving an L/D of ≥4 at 50 m s⁻¹.
- Built a component weight model that predicted 107 lb primary structure, guiding CFRP lay-ups and 7068-T6 landing-gear sizing.
- Assessed rotor acoustics and capped hover noise at ~70 dB and climb noise
- Devised risk-mitigation features—proximity sensors, emergency parachute and propeller guards—to address collision and free-fall hazards.
- Selected CFRP for the airframe and 7068-T6 aluminum for landing gear to maximize strength-to-weight and corrosion resistance.
Education
Master of Science - Aerospace Engineering
Florida Institute of Technology
Melbourne, FL05.2025
Bachelor of Science - Aerospace Engineering
University of Petroleum And Energy Studies
Dehradun, India05.2022
Skills
- Software Tools: ANSYS, SolidWorks, AutoCAD, MATLAB, Simulink
- Technical Areas: CFD, Gas Dynamics, Fluid Dynamics, Propulsion, GNC, Aerodynamics, FEA
Timeline
Engineer, Entry, Decent and Landing
NASA L'SPACE NPWEE
09.2024 - 12.2024
Academic Intern
Gnat Aviation Design Development of VTOL UAV
10.2021 - 12.2021
Master of Science - Aerospace Engineering
Florida Institute of Technology
Bachelor of Science - Aerospace Engineering
University of Petroleum And Energy Studies
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