4   Artículos

 
en línea
Tomasz Palacz and Jacek Cieslik    
The paper is part of the research aimed at determining if the vortex flow pancake (VFP) hybrid rocket engine is feasible as green in-space chemical propulsion. The objective of this study is to test an N2O/HDPE VFP hybrid ignited with N2O/C3H8 torch igni... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Olexiy Shynkarenko and Domenico Simone    
A new ignition system, based on a CH4/O2 torch has been developed by the Chemical Propulsion Laboratory of the University of Brasilia. Designed to ignite a hybrid rocket, this device has been improved to be used in testing of solid and liquid ramjet engi... ver más
Revista: Aerospace    Formato: Electrónico

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