AN OPTIMIZED HYBRID ROCKET MOTOR FOR THE SARA PLATFORM REENTRY SYSTEM DOI 10.5028/jatm.2012.04032312
This paper has described a system design process, based on a multidisciplinary optimization technique, of a conceptual optimized hybrid propellant rocket motor. The proposed engine could be a technological option for the reentry maneuvering system of the
Pedro Luiz Kaled Da Cás +3 more
doaj
Using Hydrogen Peroxide for Rocket Fuel Tank Pressurization: Innovations, Advantages, and Challenges
This paper explores the innovative use of hydrogen peroxide (H₂O₂) as a pressurizing agent for rocket fuel tanks, highlighting its potential to enhance efficiency and performance in rocket propulsion systems.
Mykhailo Vorobei, Mykola Bondarenko
doaj
Creep Prediction of Fluoroplastics Based on Physics Informed Neural Networks
Fluoroplastics are key sealing materials in rocket engines. They can easily fail due to creep during long-term storage, which may threaten the engines’ safety during operation.
Wuqi Gao, Yinan Ren, Zhidong Yang
doaj +1 more source
Liquid rocket engines occasionally experience abnormal phenomena with unclear mechanisms, causing difficulty in design improvements. To address the above issue, a data mining method that combines ante hoc explainability, post hoc explainability, and ...
Xiaopu Zhang, Wubing Miao, Guodong Liu
doaj +1 more source
Metal-organic frameworks as hypergolic additives for hybrid rockets. [PDF]
Jobin O +8 more
europepmc +1 more source
Features of paraffin-based fuel conversion for hybrid engines
The subject of this study is the evaporation and combustion processes of paraffin droplets in a gaseous medium containing an oxidant (air). Paraffin is a low-melting material that can be used as an environmentally friendly and high-energy fuel for hybrid
Svitlana Orlovska
doaj +1 more source
Swirl Injection Effects on Hybrid Rocket Motors
In the last decades, hybrid rocket engines have been increasingly studied and used in space vehicles. However, the low regression rates and specific impulses still represent major drawbacks to this technology. The objective of this study was to quantify
Susane Ribeiro Gomes +2 more
doaj
Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]
Navalino R, Muda N, Hafizah M, Ruyat Y.
europepmc +1 more source
Advancements and Limitations in 3D Printing Materials and Technologies: A Critical Review. [PDF]
Iftekar SF, Aabid A, Amir A, Baig M.
europepmc +1 more source
A Method for Real-Time Fault Detection of Liquid Rocket Engine Based on Adaptive Genetic Algorithm Optimizing Back Propagation Neural Network. [PDF]
Yu H, Wang T.
europepmc +1 more source

