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