Hybrid Propulsion Technology Development in Japan for Economic Space Launch
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
Numerical Analysis on Effect of Radiation in Laboratory-Scale Hybrid Rocket Motors
Effect of Change in Alignment of the Multiport Grain on the Performance of a Hybrid Rocket Motor
Use of N2O–O2 as the Oxidizer for the Hybrid Rocket Application
Effect of Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor
Optimal Robust Design of Hybrid Rocket Engines
Numerical Studies of Hybrid Rocket Propellant
Integrated Design-Trajectory Optimization for Hybrid Rocket Motors
Effect of Activated Charcoal on the Performance of Hybrid Rocket Motor
Mechanical Characteristics of Paraffin Wax-HTPB Based Hybrid Rocket Fuel
Virgin Galactic: Creating Safe, Reliable, and Frequent Access to Space