Detail publikace

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

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

Originální název

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

Typ

článek ve sborníku mimo WoS a Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

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

Autoři

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

Vydáno

24. 5. 2024

Nakladatel

Association Aéronautique et Astronautique de France

Místo

Glasgow, UK

Strany počet

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/"
}