Liquid propellant rocket engine cycles partially using electric turbopump-Reference-Cited by-同舟云学术

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Liquid propellant rocket engine cycles partially using electric turbopump

Published:2024-11 Issue: Volume:224 Page:138-147
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Shoyama Tadayoshi^ORCID,Wada Yutaka,Shimagaki Mitsuru,Hashimoto Tomoyuki,Takada Satoshi

Publisher

Elsevier BV

Reference17 articles.

1. Development of small centrifugal pumps for an electric propellant pump system;Johnsson;Acta Astronaut.,1990

2. Electric feed systems for liquid-propellant rockets;Pavlov Rachov;J. Propul. Power,2013

3. Optimization of hybrid upper-stage motor with coupled evolutionary/indirect procedure;Casalino;J. Propul. Power,2014

4. Comparison between the dynamic characteristics of electric pump fed engine and expander cycle engine;Zhou;Aero. Sci. Technol.,2022

5. System scheme design of electric expander cycle for LOX/LCH4 variable thrust liquid rocket engine;Liang;Acta Astronaut.,2021

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