c∗-Efficiency evaluation of transpiration cooled ceramic combustion chambers

Achievable benefits of the transpiration cooled ceramic thrust chamber are the reduction of weight and manufacturing cost, as well as an increased reliability and higher lifetime due to thermal cycle stability. The transpiration cooling principle however reduces the engine performance. In order to e...

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Veröffentlicht in:	CEAS space journal 2014-06, Vol.6 (2), p.99-105
Hauptverfasser:	Herbertz, Armin, Ortelt, Markus, Müller, Ilja, Hald, Hermann
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Technology and Astronautics Engineering Original Paper
Online-Zugang:	Volltext
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