Výsledky vyhledávání - "Catalyst chamber HTP"

THE LAST ACHIEVEMENTS IN THE DEVELOPMENT OF A ROCKET GRADE HYDROGEN PEROXIDE CATALYST CHAMBER WITH FLOW CAPACITY OF 1 KG/S

Autor: Bozic, Ognjan, Porrmann, Dennis, Lancelle, Daniel, May, Stefan

Worldwide, the hybrid rocket propulsion technology gained in importance recently. A new innovative hybrid rocket engine concept is developed at the German Aerospace Center (DLR) within the program “AHRES”. This rocket engine is based on hydroxyl-

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::51d0182ce6700697a3edb4490f25a128
https://elib.dlr.de/92816/

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