3D Printing Techniques for Paraffin-Based Fuel Grains
Comparison of Chemical Propulsion Solutions for Large Space Debris Active Removal
Effect of Activated Charcoal 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 Protrusion Configuration on Combustion Stability of Hybrid Rocket Motor
Hybrid Propulsion Technology Development in Japan for Economic Space Launch
Integrated Design-Trajectory Optimization for Hybrid Rocket Motors
Mechanical Characteristics of Paraffin Wax-HTPB Based Hybrid Rocket Fuel
Numerical Analysis on Effect of Radiation in Laboratory-Scale Hybrid Rocket Motors
Numerical Studies of Hybrid Rocket Propellant
Optimal Robust Design of Hybrid Rocket Engines
Reduced Desensitization Formulation for Optimal Control Problems
Submitted for: The Seventh IAASS Conference – Space Safety is no Accident
Suborbital company profiles, technology drivers, and mission architecture
Use of N2O–O2 as the Oxidizer for the Hybrid Rocket Application
Virgin Galactic: Creating Safe, Reliable, and Frequent Access to Space