AQUASONIC – A Sounding Rocket Based on Hybrid Propulsion
Experimental Evaluation of a Nitrous-Oxide Axial-Injection, End-Burning Hybrid Rocket
Experimental investigation of fuel regression rate in a HTPB based lab-scale hybrid rocket motor
Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets
Performance sensitivity study on a blowdown nitrous oxide paraffin wax hybrid sounding rocket
Effect of grain port length–diameter ratio on combustion performance in hybrid rocket motors
Numerical investigation on the regression rate of hybrid rocket motor with star swirl fuel grain
Ignition theory investigation and experimental research on hybrid rocket motor
Ignition of a polymer propellant of hybrid rocket motor by a hot particle
Regression rate behaviors of HTPB-based propellant combinations for hybrid rocket motor
Experimental Demonstration of the Vacuum Specific Impulse of a Hybrid Rocket Engine
Mars Ascent Vehicle Hybrid PropulsionEffort
Mars Ascent Vehicle Hybrid Propulsion Effort
Development of a Power-Efficient, Restart-Capable Arc Ignitor for Hybrid Rockets
Ablation characteristics of rocket nozzle using HfC-SiC refractory ceramic composite
Data Analysis of Hybrid Rocket Fuels Combustion Tests
Swirl Injection of Gaseous Oxygen in a Lab-Scale Paraffin Hybrid Rocket Motor
Local anomaly detection in hybrid rocket combustion tests
Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
Hybrid Propulsion Technology Development in Japan for Economic Space Launch
Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm
Conceptual Study on Low-Melting-Point Thermoplastic Fuel/Nitrous Oxide Hybrid Rockoon
Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene
High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets
Dynamic characteristics study of regression rate in variable thrust hybrid rocket motor
Clustering of paraffin-based hybrid rocket fuels combustion data
Protrusion effect on the performance of hybrid rocket with liquefying and non-liquefying fuels
Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets
Fuel-Rich Combustion with Ammonium Perchlorate Addition in a Staged Hybrid Rocket Engine
Enhancing the Regression Rate of Hydroxyl-Terminated-Polybutadiene-Based Mixed Hybrid Rockets
Effect of induced swirl flow on regression rate of hybrid rocket fuel by helical grain configuration
Experimental Visualization of Hybrid Combustion: Results at Elevated Pressures
Examining Port Geometry/Solid Loading for Additively Manufactured Fuels in Hybrid Rockets
Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage
Numerical and experimental studies of the hybrid rocket motor with multi-port fuel grain
3D Printing Techniques for Paraffin-Based Fuel Grains
Regression Rate Enhancement of Hybrid Rockets by Introducing Novel Distributed Tube Injector