[HTML][HTML] Regression Rate and Performance Analysis via Ballistic Reconstruction of a Small-Scale H2O2-Based Hybrid Rocket Fuelled by Polyvinyl Chloride

S Cassese, S Mungiguerra, R Guida, A Cecere… - Aerospace Science and …, 2024 - Elsevier
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 …

The Influence of Thrust Chamber Structure Parameters on Regenerative Cooling Effect with Hydrogen Peroxide as Coolant in Liquid Rocket Engines

C Zhou, N Yu, S Wang, S Han, H Gong, G Cai, J Wang - Aerospace, 2023 - mdpi.com
Liquid rocket engines with hydrogen peroxide and kerosene have the advantages of high
density specific impulse, high reliability, and no ignition system. At present, the cooling …

Hydrogen Peroxide Propulsion: Past Uses and Future Perspectives

A Parzybut, P Surmacz - … in Green Propulsion: Green Propellants for …, 2024 - Springer
In the realm of rocket propulsion, hydrogen peroxide has been a subject of historical intrigue
and modern fascination. This comprehensive study delves into the evolution of high …

[HTML][HTML] Upconverting thermal history paint for investigations of short thermal events

W Stryczniewicz, K Fronc, M Chojnacki… - Sensors and Actuators A …, 2024 - Elsevier
The main goal of the work was to develop phosphorescent coating for investigations of
surface temperature distribution resulted from short duration and high energy thermal events …

[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 …

[PDF][PDF] Life cycle sustainability of novel monopropellant systems

P Deroo - repository.tudelft.nl
For over 50 years, hydrazine has been the industry standard for monopropellant propulsion
systems used in space. Due to the propellant's toxicity however, the related handling and …

Specimen Design of Hydrogen Peroxide Systems for Attitude Control

A Abhishek, A Aravind, A Devak… - Acceleron Aerospace …, 2024 - acceleron.org.in
Hydrogen peroxide (HP) is one of the most desirable alternatives to hydrazine and its
derivatives, the most common type of fuel utilized in today's rocket fuel industry. Research …

Characterization of Microstructure and High-Temperature Oxidation Behaviour of Mosi2 Protective Coatings Dedicated to Mo-Based Combustion Chamber in Rocket …

E Szajna, GJ Moskal, W Stryczniewicz… - Available at SSRN … - papers.ssrn.com
This paper presents a detailed characterisation of the microstructure and high-temperature
oxidation behaviour of MoSi2 coatings obtained by pack cementation methods on a Mo …

[PDF][PDF] 低毒自己着火二液式推薬の創出とその着火及び燃焼特性に関する研究

畑井啓吾, ハタイケイゴ - 2023 - tsukuba.repo.nii.ac.jp
1957 年に旧ソ連が世界初の人工衛星であるスプートニク 1 号を打ち上げて以降,
人類は活動範囲を宇宙に拡大させてきた. 近年では, 気象衛星, 通信衛星, 測位衛星 …

超小型衛星との相性の良い多用途の推進系のシステム化と開発状況

安平浩義, 小野航大, 平山和樹, 指田春輝, 池田裕哉… - 航空宇宙技術, 2023 - jstage.jst.go.jp
抄録 This paper introduces Microsatellite-Friendly Multi-Purpose Propulsion (MFMP-PROP)
we proposed as a promising propulsion system using low-toxic propellant for microsatellite …