Boundary layer combustion of paraffin fuels for hybrid propulsion applications
Experimental analysis of SiC-based refractory concrete in hybrid rocket nozzles
Regression Rate Enhancement of Hybrid Rockets by Introducing Novel Distributed Tube Injector
Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using Oxygen/High-Density Polyethylene
Demonstration of ammonia borane-based hypergolic ignitor for hybrid rocket
Ignition and Combustion Enhancement of Boron with Polytetrafluoroethylene
Combustion Dynamics in Postchamber of Hybrid Rocket Using Radical Chemiluminescence Images
Optimal design of hybrid rocket motor powered vehicle for suborbital flight
Experimental Characterization of Combustion Instabilities in High-Mass-Flux Hybrid Rocket Engines
Numerical simulation of chemical ablation and mechanical erosion in hybrid rocket nozzle
Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics
Hybrid-Propellant Power Plant (Section 3.5)
Autoignitable and Restartable Hybrid Rockets Using Catalytic Decomposition of an Oxidizer
Enhancement of Hybrid Fuel Regression Rate Using a Bluff Body
The filling process and its effect on the start-up of electric pump in hybrid rocket motor
Brenntest DLR AHRES: 87,5% T-Stoff, HTPB, Al
Combustion performance and scale effect from N2O/HTPB hybrid rocket motor simulations
Regression Characteristics of the Cylindrical Multiport Grain in Hybrid Rockets