Tag Archives: Regression Rate

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 tvermin October 26, 2023

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

DoI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_40401144