This paper presents the development of indigenous hybrid rocket technology, using 98%
hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with …

This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket
propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid …

Conventional storable bipropellants make use of hydrazine and its derivatives as fuels and
nitrogen tetroxide as an oxidizer. In recent years, the toxicity character of these chemicals …

Today's rocket chemical propulsion systems for in-orbit use rely on toxic liquid rocket
propellants. The need for environmentally-friendly spacecraft and upper-stage high …

This paper presents a comprehensive review of the physical and chemical properties of
hydrogen peroxide as well as some regularities of its decomposition in the liquid phase …

(17) Lukasiewicz Research Network–Institute of Aviation, Center of Unmanned
Technologies, Warsaw, Poland. michal. kawalec@ ilot. lukasiewicz. gov. pl (18) Lukasiewicz …

The ignition and combustion process of a liquid fuel jet in coflow or jet in crossflow of
catalytically decomposed hydrogen peroxide hot stream for bipropellant thruster application …

В обзоре обобщены результаты исследований по разработке и изучению
характеристик гетерогенных катализаторов разложения высококонцентрированного …

Green propulsion, as an alternative for state-of-the-art toxic propellants like hydrazine and its
derivatives, is nowadays gaining attention. It is considered as a way for future sustainability …

Numerical analysis can be used to optimise design of the green propulsion thruster with
competitive costs compared to optimisation process through experiments. Furthermore, it …