Dr. B.V.S. Jyoti
Dr. B.V.S. Jyoti
Profile
Ancillary Activity
My Ancillary Activity: I am a CEO at SolvGE B.V., a spin-off from TU Delft, the Netherlands.
Biography
I am Dr.B.V.S.Jyoti, an Assistant Professor at Space System Engineering Section, TU Delft. I am also the CEO at SolvGE B.V., a spin-off from TU Delft, the Netherlands. I did my Ph.D. and Post Doctorate from KAIST, South Korea. Before coming to TU Delft, the Netherlands, I worked as a Korea Young Research Fellow in collaboration with NRF and KAIST.
Projects
Recent Project Funding:
1. DUTCH NWO Take Off -1: Funding Granted
2. TTT Voucher (TU Delft & Delft Enterprise): Funding Granted
3. Aerospace Startup Voucher (TU Delft): Funding Granted
4. DUTCH NWO Take Off -1 : Funding Granted
Past Funding:
In the past, while working in South Korea, I worked on 11 international projects.
Awards
Patents: 1. Secures 5 Patents 2. Recent Patent:
Patent Potential Topic: Innovative H2O2 Concentration Technology: Economical and Simplified In-Suit Concentration of 98%+ Hydrogen Peroxide
Inventors: B.V.S.Jyoti (PI), Jaime Quesada, & Pranav (Inventor)
Status: PCT Phase, TU Delft
Application Number: 2024229
Awards: Few of them;
- KAIST Full-time Scholarship: Sep 2011 to Feb 2015
- Excellent Ph.D. Thesis Award: Sep 2015
- Korea Research Fellowship: Oct 2015 to Feb 2018
- Outstanding Paper Award: Nov 2016
Expertise
My area of expertise is in the field of Green Propellant, Hypergolicity, and Propulsion systems.
The green propellant, hypergolicity, clean combustion, miniaturization for propulsion application are essential and current demand. I involved in these research areas for the past several years. While working in this research field, I secured 5 patents, a couple of journal publications, international conference papers and received few awards.
H2O2 is versatile as both monopropellant and oxidizer for a bipropellant or dual-mode propulsion. It can provide flexibility of required mission thrust and Isp and improve space mission capability reducing the dry weight overhead. A single propellant system serving all space propulsion missions from attitude control to orbital maneuvering would reduce the system component and weight at the economy. Moreover, lower dry weight can be converted into higher ΔV. So, this could help to achieve a low-cost, high thrust dual-mode propulsion system for space application.
I am also involved in Hydrogen peroxide printer technology to produce a wide range of H2O2 concentrations, including high concentrated H2O2, for a wide range of industrial applications including, Space Propulsion.
Expertise
Publications
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2021
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2021
Effect of parameter variation on the viscosity of ethanol gel propellants
Chloé Carer / Leonhard Xaver Driever / Stein Köbben / Max McKenzie / Fredrik Rhenman / Onno Van de Sype / Jesse van der Toorn / Casper van Wezel / Constança Miranda de Andrade Veiga / Aleksandrs Vinarskis / Botchu Vara Siva Jyoti
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2020
Design of a 1-N monopropellant thruster for testing of new hydrogen peroxide decomposition technologies
Thim Franken / Ferran Valencia-Bel / Botchu Vara Siva Jyoti / Barry Zandbergen
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2020
Hypergolicity and ignition delay study of green bipropellant system without catalyst (PPT)
Jaime Quesada Mañas / Botchu Vara Siva Jyoti / Pranav Gurumallapa
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2018
Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster
Jeongmoo Huh / Botchu Vara Siva Jyoti / Yongta Yun / M.N. Shoaib / Sejin Kwon
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Courses 2024
Courses 2023
Ancillary activities
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2022-12-09 - 2024-12-09
Industry