Development of green storable hybrid rocket propulsion technology using 98% hydrogen peroxide as oxidizer

A Okninski, P Surmacz, B Bartkowiak, T Mayer… - Aerospace, 2021 - mdpi.com
This paper presents the development of indigenous hybrid rocket technology, using 98%
hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with …

[HTML][HTML] Hydrogen peroxide–A promising oxidizer for rocket propulsion and its application in solid rocket propellants

W Kopacz, A Okninski, A Kasztankiewicz… - FirePhysChem, 2022 - Elsevier
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 …

Development of ultra-low specific speed centrifugal pumps design method for small liquid rocket engines

HI Kim, TS Roh, H Huh, HJ Lee - Aerospace, 2022 - mdpi.com
With the growth of the satellite industry, the demand for a propulsion system for small launch
vehicles and spacecraft has increased. Small liquid rocket engines may require Ultra-Low …

[HTML][HTML] Catalyst bed behavior of hydrogen peroxide/kerosene bipropellant thruster in monopropellant and bipropellant modes with cavitating venturi valve

S Kang - Acta Astronautica, 2023 - Elsevier
For typical hydrogen peroxide/kerosene bipropellant thruster applications, hydrogen
peroxide is injected into a catalyst bed prior to an injection of kerosene. During this period …

Development and coupled thruster/electrolyser tests of a water propulsion system

U Gotzig, M Wurdak, N Harmansa - Acta Astronautica, 2023 - Elsevier
Green propulsion is a key element of future Space propulsion because being
environmentally friendly is not just a legal obligation but it can significantly reduce the …

Hydrogen peroxide—a promising oxidizer for rocket engines: physical and chemical properties: decomposition in the liquid phase

AA Levikhin, AA Boryaev - Adsorption, 2024 - Springer
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 …

[PDF][PDF] Concept of a Green Propulsion System for Ioshex, Designed to Perform In-Orbit Randezvous and Docking

P Surmacz, A Parzybut, J Gramatyka… - Transactions on …, 2024 - sciendo.com
Recent challenges in space access include cost optimization and space debris reduction.
The European Space Agency has envisioned the evolution of in-orbit transportation …

Design, Modelling, and Optimisation of an Upper Stage Propulsion System for the Barracuda Sounding Rocket

JW Jodehl - 2024 - repository.tudelft.nl
Sounding rockets are used in various research applications such as micro-gravity research,
re-entry experiments and atmospheric measurements. They provide a low-cost alternative to …

Numerical Analysis of Different Injectors for Kerosene/Hydrogen-Peroxide and Ethanol Amine/Hydrogen-Peroxide for Satellite Thruster

NV Chidvilas, V Suraj, K Balaji, D Kumar - 2024 - sae.org
In a satellite thruster the function of injector plays a major role in controlling the combustion.
This paper presents the numerical simulation of two most used injectors namely, impinging …

[PDF][PDF] Development of the Liquid Green Propellants at the Lukasiewicz-Institute of Aviation

P Stężycki, P Wolański - 2023 - eucass.eu
In Europe, but also in many other countries initiative to replace toxic and corrosive rocket
propellants based on hydrazine fuels and nitrogen tetroxide oxidizers with green propellants …