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;

1. KAIST Full-time Scholarship: Sep 2011 to Feb 2015
2. Excellent Ph.D. Thesis Award: Sep 2015
3. Korea Research Fellowship: Oct 2015 to Feb 2018
4. 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.

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