Advanced Development of a Compact 5-15 lbf Lox/Methane Thruster for an Integrated Reaction Control and Main Engine Propulsion System

This paper describes the advanced development and testing of a compact 5 to 15 lbf LOX/LCH4 thruster for a pressure-fed integrated main engine and RCS propulsion system to be used on a spacecraft "vertical" test bed (VTB). The ability of the RCS thruster and the main engine to operate off...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Hurlbert, Eric A., McManamen, John Patrick, Sooknanen, Josh, Studak, Joseph W.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Spacecraft Propulsion And Power
Online-Zugang:	Volltext bestellen
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