Space Launch System Scale Model Acoustic Test Ignition Overpressure Testing

The overpressure phenomenon is a transient fluid dynamic event occurring during rocket propulsion system ignition. This phenomenon results from fluid compression of the accelerating plume gas, subsequent rarefaction, and subsequent propagation from the exhaust trench and duct holes. The high-amplitu...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Nance, Donald K., Liever, Peter A.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Launch Vehicles And Launch Operations
Online-Zugang:	Volltext bestellen
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