1. Project Management2. Resource Allocation3. QA & Regulatory Compliance4. Technology Training.Additionally, my core work involves Engine Development R&D for our reusable rocket engines. My role focuses on ensuring streamlined operations, regulatory adherence, and technological advancement.

1. Handled Complete Project Management for the Engine Development Program.2. Additionally contributed in the R&D of Injection Mechanisms and Engine design for the Re-usable Rocket Engine.

1. Designed, Developed and tested Various Injection Mechanisms suitable for Re-usable Rocket Engines.2. Worked on various combustion parameters and Engine design, nozzle optimization3. Designed software tools for complete Engine Design and parametric study for nozzle geometry design using MOC methodology.

SEARCHER MKII UAV PROJECT, Corps of EME, INDIAN ARMED FORCESDesign & Analysis of Dorsal fin for Searcher MKII UAV The aim of the project was to design and analyze the benefits of adding a dorsal fin to the current configuration of theSearcher MK II UAV and optimize the best possible geometrical parameters for fin geometry.• Designed Dorsal fin in various airfoils and inclination angles using Catia V5 software.•… Show more SEARCHER MKII UAV PROJECT, Corps of EME, INDIAN ARMED FORCESDesign & Analysis of Dorsal fin for Searcher MKII UAV The aim of the project was to design and analyze the benefits of adding a dorsal fin to the current configuration of theSearcher MK II UAV and optimize the best possible geometrical parameters for fin geometry.• Designed Dorsal fin in various airfoils and inclination angles using Catia V5 software.• CFD Analysis was done to understand and compare all configurations w.r.t default fin geometry.• Parametric Longitudinal and Lateral stability analysis was done for further inferential data.• The design with the maximum side slip angle was chosen as the final configuration to upgrade the UAV Geometry. Show less

ROTOR BLADE TIP PERFORMANCE ANALYSIS, 255 ARMY AVIATION SQDesign & Analysis of Rotor Blade Tips and Turbulence Study The aim of the project was to design and analyze a given inverted/berp foil with various blade tip geometries and carry out turbulence modelling and asses the best possible design for aerodynamic performance.• Designed tip geometries as well as various foils for comparisons and tested at various inclination angles using Catia V5 software as well as Design Modeler in… Show more ROTOR BLADE TIP PERFORMANCE ANALYSIS, 255 ARMY AVIATION SQDesign & Analysis of Rotor Blade Tips and Turbulence Study The aim of the project was to design and analyze a given inverted/berp foil with various blade tip geometries and carry out turbulence modelling and asses the best possible design for aerodynamic performance.• Designed tip geometries as well as various foils for comparisons and tested at various inclination angles using Catia V5 software as well as Design Modeler in Ansys software for the fluid domain.• CFD Analysis was done to understand and compare all turbulence data and simulated airflow characteristics.• Various parameters like Turbulent kinetic energy and Eddy viscosity as well as vorticity of the flow through streamline visualizations and contours helped us understand the best geometry suitable of the given mission requirement. Show less

Technical Roles:Team Lead, Design Projects-Worked on the following aircrafts for design projects:1. AIRBUS A330 (Galley Installation, Interior Placards)2. BOEING 767-300 (Cabin Placard Modification)3. BOEING 777-300 (NTF Carpet, Raceway Installation – LOPA)4. BOEING 757 (Cabin Floor Panels)5. AIRBUS A380 (All Exterior Placards & Markings – Installation & Production)Non-Technical Roles:Lead, Corporate Affairs- 1. Drafted MoU for AICTE-ZIEGLER… Show more Technical Roles:Team Lead, Design Projects-Worked on the following aircrafts for design projects:1. AIRBUS A330 (Galley Installation, Interior Placards)2. BOEING 767-300 (Cabin Placard Modification)3. BOEING 777-300 (NTF Carpet, Raceway Installation – LOPA)4. BOEING 757 (Cabin Floor Panels)5. AIRBUS A380 (All Exterior Placards & Markings – Installation & Production)Non-Technical Roles:Lead, Corporate Affairs- 1. Drafted MoU for AICTE-ZIEGLER collaboration2. Initiated QMS Procedure and documentation procedure for AS9100 REV D certification Head, Non-Technical Activities-Overlooked the following teams:1. R&D Team2. Business Team3. Aeroterns (Internship Recruitment)4. Webinar Team5. ZEST (Ziegler Aerospace Events & Sponsorships Team)6. Marketing TeamTraining:1. Aviation Standards & Regulations2. ASME Y14.5 2018 Regulations for Design Projects3. Project Management Show less

Worked on the following Four engines.1.GE90 (B777)2.GEnx-1B (B787) 3.PW 4056 (B747-400) 4.CFM 56 (B737, A320)• Performed complete overhaul and assembly of the above specified engines along with engine dressing.• Carried out Rig testing for CFM 56 & PW 4056 to evaluate and certify performance and engine life.• Carried out boroscopy and NDT testing for the turbine blade & compressor stages.• Studied and maintained Gearbox & APU components.