Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
01.01.2011
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Development of a Reusable Aerospike Nozzle for Hybrid Rocket Motors
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