A new system design tool for the simulation of a full hybrid rocket engine is developed in this
article. This tool enables to simulate the behaviour of the engine at different conditions …

This paper presents a computational thermo-fluid-dynamic model of the hybrid rocket
internal ballistics, which was developed with the specific aim of predicting the axial position …

The first goal of this work is to find a regression law for PVC (Polyvinyl Chloride) coupled to
hydrogen peroxide on a 10-N-scale hybrid thruster, which appears to be suitable for small …

This study presents an imaging-based deep learning tool to measure the fuel regression
rate in a 2D slab burner experiment for hybrid rocket fuels. The slab burner experiment is …

An experimental campaign was carried out on a hybrid rocket engine, using gaseous
oxygen and paraffin wax-based fuel, to investigate the effect of fuel grain length on motor …

This work presents a novel approach for the modelling of the regression rate in hybrid rocket
engines loaded with paraffin-fuel. Two different motor thrust classes have been considered …

Combustion efficiency is an important parameter of the combustion chamber. Gas injection
holes have an important influence on the mixing and combustion in solid propellant ducted …

A pseudo-two-dimensional (pseudo-2-D) model for the cylindrical combustion chamber of a
hybrid rocket is developed in this paper with the purpose of its integration in a system design …

The injection mode of oxidizer gas significantly affects the flow and heat transfer
characteristics of rocket motors with separated oxidizer and fuel propellants. In the present …

Starting from the data measured in several static firings of two laboratory-scale hybrid rocket
engines of different sizes burning gaseous oxygen with either a liquefying fuel or a …