EUCASS book series - Advances in AeroSpace Sciences

Design and tool anchoring for a 120-kilonewton expander cycle rocket engine liquid oxygen turbopump

L. Souverein, C. Maeding, T. Aichner, B. Ivancic, A. Wagner and M. Frey

Published online: 08 February 2019

DOI: 10.1051/eucass/201911591

L. Souverein

C. Maeding

T. Aichner

B. Ivancic

A. Wagner

M. Frey

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