Satellite Microthrusters where Catalysts are Fed with Green Premixed N~2O-Hydrocarbon Mixes
A Simplified Theory for Liquefying Fuel Hybrid Rocket Motor (late minute presentation)
Metallized Dual-Oxidizer Solid Propellants for Green Space Access
ADN-Based Liquid Monopropellants: Propellant Selection and Initial Thruster Development
Catalytic Decomposition of HAN-Based Monopropellant at Room Temperature over Ir/SiO~2 Catalyst
Superior Performance of Iridium Hexaaluminate Catalysts for Nitrous Oxide Decomposition
The Oxidizer Injection in Hybrid Rockets. A Means to Control Motor Performance
Catalyst Design and Catalytic Process for Space Propulsion
An Exploratory Study of Some Liquid Catalysts for Use with Hydrogen Peroxide
Towards a Reduced Kinetic Scheme for LOX/Methane Combustion
Future Hybrids and Solid Propellants for Space Applications
Small Thrusters for Microsatellites with Hydrogen peroxide as a Monopropellant
Test Bench Activities on Methane/Oxygen in DLR Lampoldshausen
Development of a Rocket Engine Igniter Using the Catalytic Decomposition of Hydrogen Peroxide
A Numerical Code for Hybrid Space Propulsion Design and Tests