Performance and Internal Flow of a Single-Stage Turbopump for Small Rocket Engines

In the development of a turbopump for rocket engines, the cost is expensive and the period is too long. We apply the gas turbine of the turbocharger for cars of a consumer product to a turbine part, and propose the turbopump for small rocket engines which adopted as the pump part the single-stage tu...

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Veröffentlicht in:	Turbomachinery 2013, Vol.41(7), pp.432-439
Hauptverfasser:	NISHI, Yasuyuki, SHIOHATA, Koki, MORISAKU, Akiyoshi, MIYAGI, Yohei, NOZUE, Tatsuhiro
Format:	Artikel
Sprache:	eng ; jpn
Schlagworte:	Cavitation Cavitation number Design analysis Impellers Internal Flow Pumps Rocket Engine Rocket engines Rockets Turbocharger Turbopump Turbopumps
Online-Zugang:	Volltext
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