Rashika S N

RASHIKA SUGGANAHALLI NATESH BABU Master’s in Space Engineering [-Ó - /- ½ Milan, Italy [-¯ https://www.linkedin.com/in/rashika-s-n-/ EDUCATION LOOKING FOR Master’s in Space Engineering ” Looking for a challenging career which demands the best of my engineering, mathematical and analytical skills and helps me in broadening and enhancing my current programming, design skills and knowledge in Aerospace domain ” Politecnico Di Milano 2018 - present ½ Milan,Italy Average: 22.8/30 B.Tech in Aerospace Engineering Alliance University 2013 - 2017 ½ Bengaluru, India TECHNICAL STRENGTH CGPA: 3.6/4.0 Intermediate college Jawahar Navodaya Vidyalaya - ½ Bengaluru , India Percentage: 86.4% UNIVERSITY PROJECTS Asteroid Redirection with Gravity Tractoring and Observation - ARGO • Space System Engineer job with International Team of 10 students. • Phase A study of a Gravity Tractoring assessment on Binary Asteroid system OS 162000. • Objective is to verify the Gravity Tractoring technique and avoid collision of Secondary Asteroid with the Earth • Designed Telecommunication Subsystem with trade-off study and risk assessment. - Telecommunication Subsystem Manager Design of Interplanetary Transfer using Gravity Assist C/C++ MATLAB Auto CAD ANSYS Arduino Board Programming MS Office Latex ERP System -IFS OpenFoam ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ MOST PROUD OF 3 Top Performer in High school Appreciation letter from minister of HRDC Government of India 3 Rajyapuraskar Award Rajyapuraskar award from The Bharat Scouts and Guides,India 3 Founding Member One of the founding member of Alliance AeroClub at Alliance University, Bengaluru, India 3 Featured in 1mwis campaign Featured in One Million Women in STEM campaign for my work in Space domain • Trajectory design of a heliocentric transfer from Earth to Mercury. • Gravity assist of Venus, to minimise delta V with resolution of Lambert’s Problem. • Two main approaches were followed, one stochastic and the other based on a nested looping function in order to spot the optimal solution in terms of Delta Budget. • Analysis of effect of perturbations on the trajectory of spacecraft was also performed. Attitude determination and control of 12U Cube-Satellite using reaction wheel and cold-gas thrusters • Designed a proper attitude control system able to keep spacecraft in a given nominal attitude. STRENGTHS • Numerical simulations using MatLab and Simulink. • Verified the dynamics, kinematics, control and perturbation models of the CubeSat. Hard-working Decision Making Motivator & Leader Amity & Optimist Conceptual Design and Performance estimation of a Sounding Rocket Dedicated and Punctual • Detailed Project management description using House of Quality and Pareto Sensitivity Analysis. Target oriented • Designed trajectory to perform experiments in Micro-gravity. • Designed the system for condition of launching and descent in Mediterranean Sea. • Performed uncertainty analysis on trajectory and recovery phases. Dedication Flexibility and Adaptability LANGUAGES B.Tech Thesis Modeling of Media Correction and Atmospheric Drag for Orbit Determination 01/02/2017 - 15/06/2017 ½ ISRO, Bengaluru, India ½ Indian Space Research Organization - Telemetry Tracking and Command Network, India • GPS delay by the Ionospheric region and Atmospheric drag. • Designed the Ionospheric media correction model - Klobuchar Model. • Usage of self-developed Klobuchar coefficients for delay computation yield better results. English Kannada Hindi Telugu German Italian HOBBIES Drawing and Painting Painting is just another way of keeping a diary R Internship Study Of Landing Gear Configurations For Light Aircraft ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ ○○○○○ É Music Addict Listen quality music of every genre ½ Council of Scientific and Industrial Research-National Aerospace Laboratories, India Reading Novels Each word has its own rhythm • Understood the various types of landing gear configurations for light aircraft. ) Volunteer Active member of of AGESCI Milano, Italy Scouts and Guides team and volunteers in various activities. Blogging Daily updates on the Space domain through my The Space Daily newsletter 22/06/2016 - 29/07/2016 ½ NAL, Bengaluru, India • Reported detailed study on Oleo-pneumatic struts and its efficiency. • Designed Telescopic helical spring struts for given load conditions. Paper Work Design and Flow Analysis Of Multi-section Variable Camber Wing • Minimizing fuel consumption is one of the major concerns in the aviation industry. • One of the methods proposed is to vary the lift-to-drag ratio of the aircraft indifferent flight conditions. • Aerodynamic characteristics of a multi-section, variable camber wing was investigated. • Proved that the multi-section variable camber wing model was providing 12 per cent change in camber from the baseline configuration. WORK EXPERIENCE External Mentor - Internship and Project Division Society for Space Education Research and Development (SSERD) 15/08/2020-Present ½ Bengaluru, India • Mentoring Interns on their project works and Conceptual mission studies. • Mentored on a Project Vulcans - Identifying Boulders on the surface of Target Asteroid and attaining a part of it to perform Water Mining Logistics Officer - Science Team Space@yourService - Mission Asclepios 28/05/2020 - Present ½ EPFL - Switzerland • Coordinating with logistics team regarding the material supply for mission. CERTIFICATES • Online certification program on "Introduction to Rocket and Satellite Engineering" from Cygnus aerospace Company in association with Valles Marineries. • Completed 2 weeks certification course on Faculty development program on "LATEX" organized by Gopalan College of Engineering and Management in association with IIT Bombay, India. • Flight laboratory training at Indian Institute of Technology, Kanpur for a period of about 20 days. • Organized and participated in one-day workshop on “Advances in Aerospace Technology” at Alliance University, India. • Online certification on "Astronomy: Discovering the Universe" course from Open 2 Study platform by Curtin University, Australia. • Team work to make Analog Astronaut mission as realistic as possible • Completed 7 days’ workshop on "Engineering Applications in Astronomy" organized by Inter-University center for Astronomy and Astrophysics, Pune, India. Graduate Apprentice Trainee • C and C++ language course from BALC Institutions, Bengaluru, India • Coordinating with the astronauts team to organize the astronauts’ trainings for each experiment. Hindustan Aeronautics Limited, HAL 05/11/2017 - 06/07/2018 ½ Aerospace Division, Bengaluru, India • Designed main parts for Indian Launch Vehicle – GSLV MK III using AutoCad platform • Introduced to ERP system –IFS (Industrial Financial System) to corporate between technical and management work. • Worked in the team of Indian Human Space Program to ensure the working of Thermal Protection system on Launch Vehicle. • Ensuring quality control requirements and safety measures at production site. REFEREES Ramesha [-R Hindustan Aeronautics Limited, Bengaluru, India Prof. Hariprasad Thimmegowda [-R Alliance University, Bengaluru, India