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- W2011182971 abstract "The EU FP7 SPARTAN project (SPAce exploration Research for Throttleable Advanced eNgine) aims at developing a highly throttleable propulsion system (10:1 thrust ratio), to perform soft and precise landing in planetary environments; the innovative technology relies on a hybrid engine burning HTPB and decomposed 87.5% H2O2 with vortex injection. In this framework the University of Padua (UPD) is responsible for developing a prompt and reliable CFD tool to support both design phases and internal ballistic analysis of the hybrid engine. To validate numerical results UPD has developed its own engine and ground testing are still ongoing to characterize hybrid performance in deep throttling. The issues related to handling and storing high concentration hydrogen peroxide have been overcome integrating the hybrid motor with a dedicated gas generator to reproduce 87.5% H2O2 in dissociated condition. The mixture produced inside the gas generator is then injected as oxidizer into the combustion chamber of the hybrid motor. This paper presents the main results of the optimization tests campaign performed on the integrated gas generator, to assess the injected hot mixture characteristics and ignition capability of the HTPB fuel." @default.
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- W2011182971 date "2013-07-12" @default.
- W2011182971 modified "2023-09-26" @default.
- W2011182971 title "Optimization of a H2O2 Gas Generator for a Hybrid Rocket Engine" @default.
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- W2011182971 doi "https://doi.org/10.2514/6.2013-4044" @default.
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