My Background

Worked as a Mechanical Design Engineer in System Integration Mechanical at Research Centre Imarat (SINT-M).

Developed conceptual, preliminary, and detailed design for avionic structures, as well as associated electromechanical systems, including battery systems and telecommunication systems such as antennas based on DFM/DFA principles.

Designed Mechanical testing systems, including Integration Jigs, Fixtures, and interface rings, for structural, thermal, and vibrational testing of avionic structures and component, as well as specialized handling beams like J-beam and lifting beams.

Designed airframes for aerospace structures to achieve a robust, resilient, and lightweight construction so that it withstands the high inertial and thermal loads while also minimizing overall weight by 30% and enhance the efficiency and range by 18%.

Performed structural analysis such as linear static and dynamic analyses for flight vehicles and interface structures exposed to substantial inertial loads. Additionally, conducted thermal design and analysis for thermal battery packages and battery mounting components with the objective of minimizing heat flow from the batteries using FEA tools such as ANSYS, ABAQUS.

Developed analytical and numerical design calculations pertaining to mechanical components, including springs, bearings, and gears. Furthermore, I conducted fastener analysis specifically focused on sectional intersection joints within a flight vehicle.

Involved and worked in all phases of product development of aero-mechanical systems including 3D and 2D drafting, prototyping, testing, qualification and manufacturing. Applied GD&T principles for drafting part and assembly drawings.

Compiled product data, design layouts and simulation data and filed reports in conformity with engineering principles and quantification. Additionally performed the Root Cause Analysis for the structures that failed in the structural tests.