MSc Astronautics and Space Engineering Tentative Weighted Average: 80/100
Main subjects include, Design and Analysis of Composite Structures, Space Propulsion, Finite Element Methods, Impact Dynamics and Spacecraft Protection, Spacecraft Attitude Dynamics and Control, Payload Engineering.
Thesis: ‘Simulation and Testing for Buckling Behavior of Deployable CFRP Booms for Large Space Structures’, DLR Braunschweig, Germany. (Also includes manufacturing of CFRP Booms).
[Feb 2010 – Jun 2010] Luleå University of Technology, Sweden (SpaceMaster Semester2)
Subjects included Spacecraft Environment Interactions, Image Processing and Remote Sensing, Optics and Radar-based Observations, Electronics in Space.
[Sep 2009 – Feb 2010] Julius-Maximilians-Universität-Würzburg, Germany (SpaceMaster Semester1)
Subjects included Spacecraft System Design, Space Dynamics, Space Physics, CANSAT Group Project.
Current recipient of Erasmus Mundus Scholarship, on basis of merit, for financing my Masters studies.
Bachelor of Technology (Hons) Aerospace Engineering GPA: 8.38/10.
Core subjects included Theory of Jet Propulsion, Aerospace Structural Analysis, Aero-elasticity, Low Speed and High Speed Aerodynamics, Computational Aerodynamics, CAD, Aircraft Stability and Control, Thermodynamics.
Thesis: ‘Study of Unstructured Grid Generations and Their Applications’
Minor Degreein Mathematics and Computing
Recipient of CBSE Merit Scholarship, on basis of my performance in AIEEE 2005(All India Rank -89).
All India Rank (AIR) 92 in Indian Institute of Technology – Joint Entrance Examination (JEE) 2005.
Supervisor: Dipl. –Ing Marco Straubel, German Aerospace Center (DLR), Braunschweig, Germany.
This on-going work aims to design a FE model using Nastran/Patran for nonlinear buckling simulations of lightweight deployable CFRP booms and perform bending tests to compare the test results with simulation results. A novel bending test rack has been designed and constructed for this purpose. The work also includes manufacturing CFRP booms and improving the manufacturing process.
Supervisor: Prof. R J Astleyand Dr. R Sugimoto, Rolls-Royce UTC in Gas Turbine Noise, Institute of Sound and Vibration Research, University of Southampton, UK.
This work compared the analytical solutions for acoustic radiation from an annular duct, developed by Prof. N Peake (University of Cambridge, UK) with the numerical results produced using ACTRAN/TM. The work is based on extending a pre-existing MATLAB code to generate an ACTRAN input file.
Supervisor: Dr. Pekka Janhunen, Senior Scientist, Finnish Meteorological Institute, Helsinki, Finland.
In this work, a basic analysis has been made on using electric sail tethers, which are component of Electric Sail Propulsion System, to find the nature of dust particles in space.
Supervisor:Prof. T.S.Sheshadri, Aeroacoustics and Plasma Dynamics Lab, Indian Institute of Science, Bangalore.
The conditions required for generation of plasma from a thin metallic wire have been studied experimentally. As part of a team, my role was to performmathematical analysis on the collected data using fast Fourier transform and wavelet transform techniques. The work finds applications in ETC Guns.Academic Projects
Activities and Interests
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