98% H2O2 and Solid Paraffin Mixed With Aluminum
Testing of Paraffin Based Hybrid Rocket Fuel Using Hydrogen Peroxide Oxidizer
Development of a Reusable Aerospike Nozzle for N2O-HTPB Hybrid Rocket Motor
Cryogenic and Lox Based Propulsion Systems
OVERVIEW ON HYBRID PROPULSION
Ignition and Combustion Characteristics of Nanoscale Metal and Metal Oxide Additives in Biofuel and Hydrocarbons
WALL PRESSURE AND THRUST OF A DUAL BELL NOZZLE
Application of Astrium's CryoROC Code to a Single Injector Problem
PERFORMANCE OF A COAXIAL SWIRL INJECTOR WITH FLOW PATH REVERSAL
ANSYS Bracket Tutorial
ANSYS 6.1 Tutorial
Propulsion System for Low Cost Approach to Space
