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Tag Archives: Regression Rate

Experimental Investigation on the Combustion Characteristics of Paraffin-based Hybrid Gas Generators

1.Events, 1.HiSST 2025, Propulsion Systems & ComponentsBy Beata Wierzbińska-PrusOctober 25, 2025Leave a comment

Zezhong WANG, Xin LIN, Xilong YU

DOI Number: N/A

Conference number: HiSST-2025-077

Thermo-Mechanical Characterization and Combustion Analysis of HTPB/Paraffin Wax Blended Hybrid Rocket

1.Events, 1.HiSST 2025, Propulsion Systems & ComponentsBy Beata Wierzbińska-PrusOctober 21, 2025Leave a comment

Rahman ABDUL, Daniele TORTORICI, Antonella INGENITO, Sasi Kiran PALATEERDHAM

DOI Number: N/A

Conference number: HiSST-2025-324

Effect of Fuel Composition and Post-Combustion Chamber length on Combustion Performance of Paraffin-based Hybrid Rocket Motor

Advanced Chemical Propulsion, HiSST 2018, Propulsion and Thrust Dynamics, Propulsion Systems and Components, Propulsion Technologies, Space PropulsionBy tverminOctober 26, 2023

Zezhong WANG  , Yi WU  , Xilong YU  , Xin LIN  , Fei Li

DoI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_40401144

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