Verification Firings of End-Burning Type Hybrid Rockets
Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene
Hybrid Propulsion Technology Development in Japan for Economic Space Launch
Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets
High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene
Combustion characteristics of the end burning hybrid rockets in laminar flow
Computational Analysis and Regression Laws for Nozzle Erosion Prediction in Hybrid Rockets
Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide
Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket
Numerical Analysis of Nozzle Erosion in Hybrid Rockets and Comparison with Experiments