Direct Evidence of Spatial Burning Rate Variation as Cause of Midweb Anomaly

With the use of the ultrasonic pulse-echo technique, local burning rates are measured at different radial locations across the web during static tests of center-perforated solid propellant rocket motor grains. The measurement shows a higher burning rate in the midweb region and a lower burning rate...

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Bibliographische Detailangaben

Veröffentlicht in:	Journal of propulsion and power 2001-03, Vol.17 (2), p.449-452
Hauptverfasser:	Deepak, Desh, Jeenu, R, Sridharan, P, Padmanabhan, M. S
Format:	Artikel
Sprache:	eng
Schlagworte:	Burning rate Combustion Computer simulation Pressure effects Rocket engines Ultrasonic measurement
Online-Zugang:	Volltext
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