Paraffin-based hybrid rocket engines applications: A review and a market perspective

A Mazzetti, L Merotto, G Pinarello - Acta Astronautica, 2016 - Elsevier
Hybrid propulsion technology for aerospace applications has received growing attention in
recent years due to its important advantages over competitive solutions. Hybrid rocket …

Bridging the technology gap: Strategies for hybrid rocket engines

C Glaser, J Hijlkema, J Anthoine - Aerospace, 2023 - mdpi.com
Hybrid rocket propulsion, first demonstrated by the Russian GIRD-09 rocket in 1933,
combines liquid oxidizer and solid fuel for thrust generation. Despite numerous advantages …

Three-dimensional numerical modeling of a rocket engine with solid fuel

AG Kushnirenko, LI Stamov, VV Tyurenkova… - Acta Astronautica, 2021 - Elsevier
This paper presents three-dimensional numerical modeling of the processes occurring in the
combustion chamber of a hybrid engine. Numerical simulation using verified author's code …

A new strategy for the reinforcement of paraffin-based fuels based on cellular structures: The armored grain—Mechanical characterization

R Bisin, C Paravan, S Alberti, L Galfetti - Acta Astronautica, 2020 - Elsevier
Paraffin waxes have been identified as promising hybrid rocket fuels. Though attractive from
the ballistic point of view, these materials feature poor mechanical properties and, in …

Numerical simulation of combustion surface regression based on Butterworth filter in hybrid rocket motor

X Meng, H Tian, X Chen, X Jiang, P Wang, T Wei… - Acta Astronautica, 2023 - Elsevier
This paper provides a valuable method to perform transient numerical simulations for hybrid
rocket motors (HRMs). A two-dimensional transient numerical simulation model based on …

Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain

Z Zhang, X Lin, Z Wang, K Wu, J Luo, S Fang, C Zhang… - Acta Astronautica, 2022 - Elsevier
The combustion characteristics obtained from the coupling effect between swirl injection and
a novel composite hybrid rocket fuel grain were investigated. The novel composite fuel grain …

Dynamic characteristics study of regression rate in variable thrust hybrid rocket motor

H Tian, X Meng, H Zhu, C Li, R Yu, Y Zhang, G Cai - Acta Astronautica, 2022 - Elsevier
This paper aims at the dynamic characteristics study of variable thrust HRMs, for which a two-
dimensional transient numerical model of HRM is established. Complete transient …

Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure

Z Wang, X Lin, F Li, X Yu - Aerospace Science and Technology, 2020 - Elsevier
The combustion performance of a novel fuel grain having a nested helical structure was
experimentally investigated using a laboratory-scale hybrid rocket engine. This grain …

Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades

D Qu, X Lin, K Zhang, Z Li, Z Wang, G Liu… - Virtual and Physical …, 2023 - Taylor & Francis
Hybrid rocket engines suffer from the restricted mechanical properties and low regression
rates of current polymeric fuel grains. We propose a three-dimensional printed aluminium …

High regression rate hybrid rocket fuel grains with helical port structures

SA Whitmore, SD Walker, DP Merkley… - Journal of Propulsion and …, 2015 - arc.aiaa.org
Results from a development campaign, where modern additive manufacturing methods are
used to fabricate hybrid rocket fuel grains with embedded helical ports, are presented. The …