Sahil Thakur

Phone : +91-821*******

Email : adhl8e@r.postjobfree.com

LinkedIn URL:

https://www.linkedin.com/in/sahil-thakur-0119b2152

CAREER OBJECTIVE

A highly-motivated, hardworking engineering student aspiring to develop a career as a Aerospace Avionics Engineer to help use the sciences for the betterment of the society and overall quality of life around us. My short term goal is to secure a challenging position in a reputable organization to expand my learnings, knowledge, and skills. My long term goal is to see myself at a key position handling important portfolios. My definitive objective is to team up with the pioneers of a similar field, gain from them, have the option to work close by them and use the tremendous capability of the techniques and innovation that

have been found and those that are yet to be found in a manner that can continue our ages to come.

ACADEMIC BACKGROUND

Year

Qualification – Degree / Diploma / Certificate

Board/University

College

/ Institute/ University

Percentage / CGPA

2015

Class 10th

Himachal Pradesh Board

S.P.S. Barchhwar

86.2

2017

Class 12th

Himachal Pradesh Board

S.P.S. Barchhwar

76

2017-2021

B Tech

University

University of petroleum and energy studies, dehradun

7.0

PROJECTS

Project Title: Development of Hall Thruster

[ Selected for International Astronautical Congress 2020 ]

Duration: August,2019 – May,2020

Learning Outcome:

This project focuses on the development of a small scaled hall effect microthruster, utilizing inert and non-contaminating xenon gas as propellent. Hall thruster uses a cross field discharge as explained by hall effect to generate plasma. A perpendicular electric and magnetic field application accelerates ions to high exhaust velocities and the transverse magnetic field allows electrons to traject such that they neutralize the electric field. Observing that hall thrusters give a higher thrust for a specific power input, this project focuses on increasing the efficiency at the same power input. Reducing the power requirements by implementing lower power consuming radial magnetic field ™and axial electric field is an additional advancement. Considering scalability, one of the major concerns is to bring changes in the conventional structure design such the size and weight are reduced. Both the anode and cathode are thus used for propellent injection although from cathode the quantity might be significantly low. The materials so far chosen are stainless steel for anode, barium oxide for cathode and borosil for wall of plasma chamber.

Result:

We have designed a hall thruster for 127mN thrust.

For ionization we are using Electron bombardment technique.

We are using Xenon gas as propellant.

Specific impulse is 1765.

discharge voltage is 350V.

Power requirement is 2.2kW.

Electric field is 18.773 KV/m and Magnetic field is 116.508565 gauss.

Thermal and Structural analysis is also done.

Project title: Detection of targets using SAT datasets

(Research in progress)

TRAININGS & CERTIFICATIONS

Internship project: Low Power wireless communication technologies and comparison range.

Company: Okulo Aerospace

Objective: The prime objective of this project is to apprehend, experience and realise the obstacles faced during Low Power Wireless communication technologies for enhanced understanding of Wireless Communication systems, thereby exploring peaks of advancement and scope in near-future technologies. Wireless communication systems that incorporate unmanned airborne vehicles guarantee to give savvy remote availability to gadgets without foundation inclusion. Contrasted with terrestrial communications or those dependent on high-altitude platforms on-request wireless systems with low-elevation UAVs are by and large quicker to convey, all the more deftly re-designed, and are probably going to have better correspondence channels because of short-range line-of-sight links. Be that as it may, the usage of exceptionally versatile and vitality obliged UAVs for wireless communication likewise presents numerous new difficulties. In this project, we identified various technologies used in drone communication and compared the products (Transmitter, Receiver, Transponder etc.) which are using in Wireless Communication Technologies (Long-Term Evolution (LTE), Radio-Frequency (RF), Low Power Wide Area Network (LoRaWAN),Satellite Communication (SATCOM) ) on different parameters.

Result: We compared different products and different techniques for wireless communication technologies and found that Radio Frequently technique is best for drone communication.

Certificates:

Quadcopter UAV

Gas turbine

Airfoil designing

Arduino course

TECHNICAL SKILLS

Programming Languages : C, Python (beginner), MATLAB (Beginner)

Tools & Technologies: CATIA V5 (beginner)

CO-CURRICULAR ACHIEVEMENTS

Personality enhancement program.

87th rank Holder in 10th result (Himachal Pradesh board)

Core committee member of infinity space club.

Research paper selected in International Astronautics Congress (2020)

Venture ideation

Design thinking

EXTRA-CURRICULAR ACHIEVEMENTS

Player Kabaddi at State level

Awarded as best stand-up comedian

Infinity space club core member

PERSONAL DETAILS

Date of Birth: 16, August,2020

Permanent Address: Village- Bakarta, P.O.- Rakhoh, Tehsil- Sarkaghat, District- Mandi (Himachal Pradesh)

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