Publication detail

DESIGN, DEVELOPMENT, AND TESTS OF THE E-PUMPS FOR THE RELIANCE ENGINE

KOZÁK, J. VÁŇA, P. HORKÝ, J. MACHOŇ, M. ŠTEFAN, D.

Original Title

DESIGN, DEVELOPMENT, AND TESTS OF THE E-PUMPS FOR THE RELIANCE ENGINE

Type

article in a collection out of WoS and Scopus

Language

English

Original Abstract

The electric-pump-fed system of the rocket engine represents an important innovation in the field of rocket propulsion. While the general concept itself is already several decades old, the technology was not still adopted in the commercial applications on a large scale. The exception being the Rutherford engine developed by RocketLab. Nonetheless, rapid development of the technologies critical for the electric pump-fed systems sets the bright future of this concept.

Keywords

ELECTRIC PUMP, HIGH SPEED MOTOR, STORABLE PROPELLANTS, DYNAMIC FLOW CONTROL, MOTOR INVERTER

Authors

KOZÁK, J.; VÁŇA, P.; HORKÝ, J.; MACHOŇ, M.; ŠTEFAN, D.

Released

24. 5. 2024

Publisher

Association Aéronautique et Astronautique de France

Location

Glasgow, UK

Pages count

11

URL

https://www.3af-spacepropulsion.com/

BibTex

@inproceedings{BUT188800,
  author="Jiří {Kozák} and Petr {Váňa} and Jan {Horký} and Matěj {Machoň} and David {Štefan}",
  title="DESIGN, DEVELOPMENT, AND TESTS OF THE E-PUMPS FOR THE RELIANCE ENGINE",
  year="2024",
  pages="11",
  publisher="Association Aéronautique et Astronautique de France",
  address="Glasgow, UK",
  url="https://www.3af-spacepropulsion.com/"
}