Development of a high flow rate piston pump for rocket engines

There is a need for cheaper small satellite rocket launchers. One way of reducing costs is to reduce the cost of individual components. We describe here the development of an inexpensive piston pump for rocket engine applications. It demonstrates that it can deal with the combined requirements of hi...

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Veröffentlicht in:	Journal of physics. Conference series 2018-08, Vol.1065 (26), p.262003
Hauptverfasser:	Augousti, A T., Baker, A, Claus, M, Karaveckas, L
Format:	Artikel
Sprache:	eng
Schlagworte:	Cryogenic temperature Flow velocity Physics Rocket engines Rocket launchers Small satellites
Online-Zugang:	Volltext
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