Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine

Autor
Keine Angabe
Verlag
Hutson Street Press
Veröffentlicht
20250522
ISBN
9781025091464
ISBN-Registrierungsgebiet
Englischsprachiger Raum (ISBN 978-1)

Beschreibung

The design of a pump intended for use with a dual expander cycle (LOX/H2) engine is presented. This arrangement offers a number of advantages over hydrogen expander cycles; among these are the elimination of gearboxes and inter-propellant purges and seals, an extended throttling range, and higher engine operating pressures and performance.