session IPB

1

Prospects in green propellants and green propulsion systems

10

withdrawn

Prof. Rachid Amrousse

Chouaib Doukkali University

Morocco

2

Student built cryogenic liquid rocket engine technology demonstrator: Results and learning outcomes

10

withdrawn

Ms. Francesca van Marion

Delft Aerospace Rocket Engineering (DARE)

The Netherlands

3

Overview of existing launch vehicle fuel tank pressurization systems and development prospects

10

Mr. Vadym Khomiak

Yuzhnoye State Design Office

Ukraine

4

A Trade Study of Mission Architectures for Centrifugal Nuclear Thermal Propulsion

10

confirmed

Mr. William Ziehm

University of Alabama in Huntsville

United States

5

Toolkit for Liquid Rocket Propulsion System Design

10

confirmed

Mr. Nijat Abdulla

National Aviation Academy - Azerbaijan

Azerbaijan

6

Design evaluation of the performance capabilities and schematic for the LOx/LNG liquid-propellant rocket engine

10

Dr. Volodymyr Shulha

Yuzhnoye State Design Office

Ukraine

7

A new H2O2 oriented Rocket and Satellite Propulsion Laboratory Center

10

confirmed

Mr. Lukasz Radzikowski

Łukasiewicz Research Network – Institute of Aviation (ILOT)

Poland

8

Using the intrinsic magnetic susceptibility change of methane combustion to increase maneuverability of RCEs

10

Mr. Akash Prasanna

R V College of Engineering, Bengaluru

India

9

Numerical simulation of a detonation engine

10

confirmed

Ms. Elena Mikhalchenko

Scientific Research Institute for System Analysis, Russian Academy of Sciences (RAS)

Russian Federation

10

Power converter with high gain, high performance for space thrusters based on electrospray technology.

10

Mr. Francisco José Blázquez Plaza

Universidad Carlos III de Madrid

Spain

11

Green Propellants: Self-Pressurization Behavior Modelling

10

confirmed

Mr. Simone La Luna

Politecnico di Milano

Italy

12

exploring the complexities of pintle injectors for high performance rocket propulsion an advanced numerical simulation investigation with expansion deflection nozzle

10

confirmed

Mr. Sudarsan Nerella

University of Petroleum and Energy Studies

India

13

Report on test firing results of 6.5 kN pressure-fed hypergolic storable liquid rocket engine and comparison to the design theoretical calculations.

10

confirmed

Dr. Florin Mingireanu

Romanian Space Agency (ROSA)

Romania

14

structural modification and flow analysis of isolator for enhanced efficiency of dual mode ramjet-scramjet engine

10

confirmed

Mr. Greekshith Mahesh Babu

R V College of Engineering, Bengaluru

India