Microstructural and ablative properties of graphite nozzles with SiC coating deposited by CVD technique

Microstructural and ablative properties of graphite nozzles with SiC coating deposited by CVD technique

The development of efficient, reliable and affordable propulsion units is one of the main objectives in the development of aerospace technology. Typically the final cost of the vehicle is deeply affected by this subsystem. In this study, a hybrid combination of the ablative chamber is presented wher...

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Podrobná bibliografie
Hlavní autoři: Oswaldo B Loureda, Felipe Rocha Caliari, Inácio Regiani, Felipe de Souza Miranda, Roberson José da Silva, Gilberto Petraconi Filho
Médium: Článek
Jazyk:English
Vydáno: IOP Publishing 2020-01-01
Edice:Materials Research Express
Témata:
rocket engines
ablation test
SiC coating
plasma torch
On-line přístup:https://doi.org/10.1088/2053-1591/ab6c87

Internet

https://doi.org/10.1088/2053-1591/ab6c87

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