36   Artículos

 
en línea
Jan Erik Zeriadtke, Joël Martin and Viola Wartemann    
The performance of hybrid rocket engines is significantly influenced by the fuel geometry. Burnback simulations, to determine the fuel surface and fluid volume, are therefore an important tool for preliminary design. This work presents a method for the s... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Christopher Glaser, Jouke Hijlkema and Jérôme Anthoine    
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, such as enhanced safety, controllability, and potential environmental benefits... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Christian Paravan, Anwer Hashish and Valerio Santolini    
Hybrid rocket engines (HREs) offer a low-cost, reliable, and environmentally friendly solution for both launch and in-space applications. Hybrid propellants have been identified as green thanks to their use of non-toxic, non-carcinogenic oxidizers. Of pa... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Giovanni Fasulo, Luigi Federico, Adolfo Sollazzo, Luciano De Vivo and Roberto Citarella    
A rocket?s turbulent jet radiates intense acoustic waves, which are an acoustic load for structural components like payload, launch structure, and rocket avionics, and impact communities near the launch site. Therefore, a careful characterization of the ... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Jihyoung Cha    
This study deals with the mathematical modeling and numerical simulation of chemical propulsion systems (CPSs). For this, we investigate and summarize a comprehensive collection of the simulation modeling developments of CPSs in academic works, applicati... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Yang Liu, Xintong Li, Pengcheng Wang, Xiaotian Zhang, Hao Zhu and Guobiao Cai    
This paper proposed a multi-objective, multi-disciplinary design optimization and multi-attribute evaluation method for the manned lunar lander descent stage. A system design model is established considering multiple disciplines such as propulsion, struc... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lorenzo Casalino, Andrea Ferrero, Filippo Masseni and Dario Pastrone    
Hybrid rocket engines are a green alternative to solid rocket motors and may represent a low-cost alternative to kerosene fueled rockets, while granting performance and control features similar to that of typical storable liquid rocket engines. In this w... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Tor Viscor, Landon Kamps, Kazuo Yonekura, Hikaru Isochi and Harunori Nagata    
An understanding of the scalability of hybrid rocket regression models is critical for the enlargement and commercialization of small-scale engines developed within universities and similar research institutions. This paper investigates the fuel regressi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lorenzo Casalino, Filippo Masseni and Dario Pastrone    
Optimization of Hybrid Rocket Engines at Politecnico di Torino began in the 1990s. A comprehensive review of the related research activities carried out in the last three decades is here presented. After a brief introduction that retraces driving motivat... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lorenzo Casalino, Filippo Masseni and Dario Pastrone    
The optimal design of the propulsion system for a potential Mars Ascent Vehicle is analyzed, in the context of the Mars Sample Return Mission. The Mars Ascent Vehicle has to perform an initial ascent phase from the surface and then circularize into a 170... ver más
Revista: Aerospace    Formato: Electrónico

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