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 …

This paper presents the topic of using solid rocket propulsion for de-orbiting spacecraft, in
order to fulfil space debris mitigation requirements. The benefits and disadvantages of using …

Low-thrust, end-burning solid rocket motors have applications as propulsion systems for a
class of small, transonic, uncrewed aerial vehicles. This paper provides new experimental …

Dispersed metallic fuels are energy-intensive components of various gel-like and composite
solid propellants, which significantly improve the performance of propulsion systems. This …

The rheological properties and isothermal curing kinetics of the GAP/AN/HMX propellant
slurries were investigated by steady rheological measurements and isothermal rheological …

This paper presents the results of an experimental study of the processes of thermal
decomposition and ignition of high-energy materials (HEMs) containing an oxidizer, a …

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

This paper presents scientific merits and design challenges associated with a novel idea to
perform rocket sounding of the Martian atmosphere. Limited data sets of the Mars …

Дисперсные металлические горючие являются энергоемкими компонентами различных
гелеобразных и смесевых твердых топлив, существенно повышающими …

Представлены результаты экспериментального исследования процессов термического
разложения и зажигания высокоэнергетических материалов (ВЭМ), содержащих …