Hybrid Propulsion Technology Development in Japan for Economic Space Launch
3D Printing Techniques for Paraffin-Based Fuel Grains
Submitted for: The Seventh IAASS Conference – Space Safety is no Accident
Comparison of Chemical Propulsion Solutions for Large Space Debris Active Removal
Suborbital company profiles, technology drivers, and mission architecture
Effect of Change in Alignment of the Multiport Grain on the Performance of a Hybrid Rocket Motor
Numerical Analysis on Effect of Radiation in Laboratory-Scale Hybrid Rocket Motors
Effect of Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor
Use of N2O–O2 as the Oxidizer for the Hybrid Rocket Application