Engineering Engineer
Resume:
Mary Sharon Rose Bondugula
Aerospace Engineer
Highly motivated, versatile, go-getter with a background in Aerospace Engineering. A perfect balance of analytical and interpersonal skills to work in anyrole. Passionate about constantly learning and driving operational efficiency. Areas of Interest: Space Propulsion Aerospace Materials Space Dynamics Orbital Mechanics Integration of Nanotechnology in Aerospace Engineering. marysharon.bondugula@mail
.polimi.it
Milan, Italy
linkedin.com/in/sharon-rose-
173554151
SKILLS
Communication,
Problem Solving
Teamwork
Continuous Learner
Self-Management
Planning
PUBLICATIONS
paper publication
Investigation of Ignition
Delay of Hydrocarbon
Fuels using Shock Tube
2018
International Journal of Pure
and Applied Mathematics
Volume 118 No. 20 2018,
3687-3692
VOLUNTEER
EXPERIENCE
Volunteer at
National Service
Scheme
Karunya Institute of
Technology and
Sciences
06/2014 - 06/2015,
India
WORK EXPERIENCE
Student Trainee
Bharat Heavy Electricals Limited
06/2017, Hyderabad,India
Studied about the components and classification of Gas Turbine Engine. Stress analysis of this Engine,Test facilities to test various engine
Student Intern
Hindustan Aeronautics Limited, AERDC (Engine Division) 05/2017, Bangalore, India
Studied on design and development of Piston Engines, Turbo-Jet Engines, Jet Fuel Starter, etc. The major propulsion sub technology area where it has expertise is the Aero-Thermo-Dynamic EDUCATION
M.Sc in Space Engineering
Politecnico di Milano
09/2018 - Present, Milan,Italy
Thesis: Manned Spacecraft Design
B.Tech in Aerospace Engineering. 8.8/10
Karunya Institute of Technology and Sciences (Deemed to be University) 06/2014 - 07/2018, Coimbatore, Tamilnadu
Thesis: Investigation of Ignition Delay of
Hydrocarbon Fuels using Shock Tube
TECHNICAL SKILLS
SOFTWARES Matlab, CATIA, SolidWorks, ANSYS (FEM & CFD), XFLR5, AutoCAD, Latex, C
(Programming Language), Microsoft Office Suite.
RESEARCH AREAS
Payload Design- Remote Sensing for Detection and Monitoring of Wildfires
(02/2020 - 07/2020)
Mission is designed to detect wildfires anywhere in the world before anyone else. With a revisit time having one hour at most and global coverage, the aim of the mission is to improve on previous mission's efforts to provide firefighters with precise and quick data and aid them in their mission to extinguish wildfires. The goals of high resolution, extremely low revisit time and global coverage was achieved with a constellation consisting of a large number of satellites. Softwares used: SPENVIS WinLens 3D Inventor Ansys Matlab Achievements/Tasks
Achievements/Tasks
Orbital Mechanics, Space Propulsion, Combustion Processes in Thermochemical Propulsion, Spacecraft Attitude Dynamics & Control, Aerospace Technologies& Materials, Dynamics and Control of Space Structures, Payload Design.
Aerodynamics, Computational Fluid Dynamics, Rocket Propulsion, Advance Space Dynamic, Aircraft Systems, Finite Element Analysis in AerospaceApplication, Materials in Aerospace Application. Page 2 of 2
VOLUNTEER
EXPERIENCE
Student Volunteer
at Music Club
Karunya Institute of
Technology and
Sciences
01/2016 - 05/2016,
India
Student Volunteer
at Red Cross Youth
Karunya Institute of
Technology and
Sciences
07/2015 - 12/2015,
India
AWARDS
Second position in
Parachute designing
(National level tech-fest);
Mindkraft National level
Techno-Management fest
(03/2017)
Karunya Institute of Technology
and Sciences
Theory of Music Award
(12/2014)
Trinity College London
INDUSTRIAL
VISITS
Liquid Propulsion System
Centre, Mahendragiri,
Kanyakumari (02/2016)
Conference/Issuer of the
certificate
Vikram Sarabhai Space
Centre,
Thiruvananthapuram
(09/2016)
Conference/Issuer of the
certificate
RESEARCH AREAS
Star Pointing and De-Tumbling of 16U CubeSat in the Low Earth Orbit- ADCS
(09/2019 - 05/2020)
This project is to develop a preliminary design of the attitude control system of the 16U satellite category and design a simplistic control laws to satisfy basic phases involved in cubesat’s life i.e., de-tumbling and tracking a Local vertical Local Horizontal (LVLH) frame or i.e., pointing at the desired direction. Attitude Sensors: Gyroscope, Magnetometer and Sun Sensor Actuators: 3 Magnetic Torquers & 4 Control Moment Gyros Altitude: 600Km
Mining Near Earth Asteroid Systems (Miners) - Project proposal for funding by the European Commission (03/2019 - 06/2019)
The project aim is to develop a small spacecraft that could land on NEAs and survey to identify the useful materials in asteroids before preparing a practical mining mission. Proposed and analysed a mission focusing on the utilisation of small spacecraft for the entire asteroid mining cycle. This includes prospecting, mining, and return of relevant substances. INTERPLANETARY EXPLORER MISSION (Transfer from Earth to Mercury using a gravity assist of Venus) (11/2018 - 02/2019)
• The trajectory has been designed with the intent to minimize the overall deltaV required using the resolution of a Lambert’s problem for the characterization of the heliocentric transfers and using a patched-conics method to model the fly-by maneuver. • Optimized Interplanetary phases of minimum delta-V by use of Pork-chop analysis in Matlab.
Planetary Explorer Mission- Orbit Analysis, Ground Track Estimation and Effects of Orbit Perturbations. (10/2018 - 01/2019)
The ground track is characterised and are proposed variations of the semi-major axis of the orbit necessary to reach a repeating ground track, to improve communications with groundFinally, a satellite is selected in the same orbital The evolution of its orbital elements is compared with the values obtained propagating the orbit using our model.
Investigation of Ignition Delay of Hydrocarbon Fuels using Shock Tube, Final Bachelor's Thesis (09/2017 - 05/2018)
The present study of ignition delay is concerned with ethane and The measurement of ignition delay times have been made behind the reflected shock region in the temperature range of 800-2200 K and in the pressure range of 9-40 atm at equivalence ratios (ф = 5 & 1). Aircraft Design Project (07/2017 - 10/2017)
A 5-seater business jet engine aircraft cruising at M=0.7 at 14Km altitude is considered. The final design stays true to the desired considerations of a long range aircraft that can provide high fuel efficiency as well. SOFTWARE USED: XFLR5 (Analysis tool)
Increase in Ignition using Aluminium Oxide Nano-Particle (07/2016 - 10/2016) Synthesis of Aluminium Oxide Nano-Particle by adding Urea to Aluminium Nitrate and heating it in muffle furnace at 6000C. Finding size and volume fraction and other properties of the nano-particle. Characterisation through XRD
CERTIFICATES
Cambridge English Language Assesment, ESOL International (12/2014) Italian Language Course Basic Level, Foreign Language Institute (04/2018 - 05/2018) Course on CATIA, CAD Solutions (09/2016 - 11/2016) Fuel Cell and Hybrid Vehicle Technology, SAE Group (11/2016) Composite Materials in Aerospace Applications, Airframe Aerodesigns Pvt Ltd (AAPL)
(02/2016)
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