Utility of Multiprotrusion as the Performance Enhancer in Hybrid Rocket Motor
Use of N2O–O2 as the Oxidizer for the Hybrid Rocket Application
Protrusion effect on the performance of hybrid rocket with liquefying and non-liquefying fuels
Measurement of regression rate in hybrid rocket using combustion chamber pressure
Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels
Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying Ratio
Enhancing the Regression Rate of Hydroxyl-Terminated-Polybutadiene-Based Mixed Hybrid Rockets
Enhancement of Hybrid Fuel Regression Rate Using a Bluff Body
Effect of protrusion on the enhancement of regression rate
Effect of Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor
Effect of multi-location swirl injection on the performance of hybrid rocket motor
Effect of Change in Alignment of the Multiport Grain on the Performance of a Hybrid Rocket Motor
Effect of Activated Charcoal on the Performance of Hybrid Rocket Motor