Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets

Autor:	Yuji Saito, Kentaro Soeda, Yushi Okutani, Harunori Nagata, Ayumu Tsuji, Masaya Kimino
Rok vydání:	2018
Předmět:	020301 aerospace & aeronautics Materials science 0203 mechanical engineering High pressure 0103 physical sciences Regression rate 02 engineering and technology Mechanics 01 natural sciences 010305 fluids & plasmas
Zdroj:	2018 Joint Propulsion Conference.
DOI:	10.2514/6.2018-4529
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::14131b6d93d9e112e2369b12f7f3ec93 https://doi.org/10.2514/6.2018-4529 Zobrazit plný text záznamu