Dipl.-Ing. Saravanan Sudalayandi

The main objective of the project is to design, analysis and fabrication of the instrument. I am working as a Mechanical Design Engineer. I am responsible for designing the instrument setup using the design software CATIA V5 and vibrational analysis are done in ANSYS and NX Nastran. The project is proposed by the ESA with joint collaboration of NASA, DLR and IRS. The optical instrument is used to observe the explosion and defragmentation of the ATV-5 re-entry vehicle. http://atv5.seti.org/index.html

The main objective of the project is to design and analysis of thruster integration for UWE-4. I am responsible for the design and development of the thruster integration. I worked as a Mechanical Design Engineer. I designed the thruster using the design software CATIA V5 and structural, vibrational and thermal analysis are done in ANSYS.

The main objective of the project is to design analysis and fabrication of GIMBAL with moving mass for the Nano Satellite. I am responsible for the design and development of the gimbal. I worked as a Mechanical Design Engineer. I designed the Gimbal using the design software CATIA V5 and structural analysis are done in ANSYS. And also responsible for preparing the G-code for 2D-CNC machine. Fabrication are done in the 2D- CNC machine and 3D printer.

The main objective of the project is to develop an Unmanned Aerial vehicle (UAV), with vertical takeoff and landing capabilities (VTOL) mainly intended for ground surveillance .The main theme of this project is the tilt mechanism. I was mainly responsible for the design development and the fabrication of the UAV. The design and analysis was done in the software CATIA V5, Fluent and ANSYS. I am the Team Leader among the Group of four.

The main objective of the project to analysis and to do the Quality Inspection of the ADOUR MK -871 Jet Engine. I was responsible for the analysis of the turbine blades and its components using the ANSYS Software. I am the team member in the quality inspection team to check the quality of the turbine blades. And NDT testing are done over it.

The main objective of the project is to develop a structural modification and analysis over the GSLV and PSLV rockets. The design and analysis is carried out CATIA V5 and ANSYS software. And documentation are done according to ISRO and FAA regulations

Robotics, Advanced automation and control, Team design project, Seminar in (Multi-robot coordination in complex environment with task and communication constraints), Space physics, Spacecraft system and design, Space dynamics, Can sat (1D satellite design).

Space physics, Spacecraft Enviromental Interactions, Space Electronics, Optics and Radar Technology

AUTO-CAD, CATIA, PRO-E, ANSYS, NX-CAD, Soildworks, GD&T, MSP, PPM.

Propulsion, Aerodynamics, Aircraft structures, Avionics, CFD, FEM.