Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor
Ignition of a polymer propellant of hybrid rocket motor by a hot particle
Swirl Injection of Gaseous Oxygen in a Lab-Scale Paraffin Hybrid Rocket Motor
Performance sensitivity study on a blowdown nitrous oxide paraffin wax hybrid sounding rocket
Experimental Demonstration of the Vacuum Specific Impulse of a Hybrid Rocket Engine
Numerical investigation on the regression rate of hybrid rocket motor with star swirl fuel grain
Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets
Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
Hybrid Propulsion Technology Development in Japan for Economic Space Launch
Ablation characteristics of rocket nozzle using HfC-SiC refractory ceramic composite
Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm
Data Analysis of Hybrid Rocket Fuels Combustion Tests
Effect of induced swirl flow on regression rate of hybrid rocket fuel by helical grain configuration
Clustering of paraffin-based hybrid rocket fuels combustion data