Experimental evidence of H2/O2 propellants powered rotating detonation waves

The paper presents experimental evidence of continuous detonation in a rotating detonation rocket engine (RDRE) powered by H2/O2 propellants. High-speed chemiluminescence imaging is used to characterize the detonation wave dynamics by introducing a tracer in the hydrogen fuel flow. The results show...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Combustion and flame 2020-04, Vol.214, p.136-138
Hauptverfasser:	Sosa, Jonathan, Burke, Robert, Ahmed, Kareem A., Micka, Daniel J., Bennewitz, John W., Danczyk, Stephen A., Paulson, Eric J., Hargus, William A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Chemiluminescence Detonation waves Flow velocity Hydrogen fuels Propellants Rocket engines Rotation Upper stage rocket engines
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!