Skip to main content
Fachgebiete
Automobil + Motoren Bauwesen + Immobilien Business IT + Informatik Elektrotechnik + Elektronik Energie + Nachhaltigkeit Finance + Banking Management + Führung Marketing + Vertrieb Maschinenbau + Werkstoffe Versicherung + Risiko
DE
EN
Bücher
Zeitschriften
Themenseiten
Organisationspsychologie Projektmanagement Marketing Smart Manufacturing
Weitere Formate
Podcasts Webinare Technik Webinare Wirtschaft Kongresse Veranstaltungskalender Awards
Jetzt Einzelzugang starten
Zugang für Unternehmen
Referenzkunden
SLX-Digitalkonferenz: Zukunftswerkstatt 2024

Mehr Umsatz mit Top-Kontakten

Am 7. Mai erfahren Sie, wie Vertriebsteams Leadgenerierung, Leadnurturing und Leadstrategien effizient steuern können.
Erweiterte Suche
Anmelden
nach oben
Erschienen in:
Gaussian Process-Based Feedback Linearization Control for Quad-Tiltrotor Kapitel lesen Erstes Kapitel lesen

2023 | OriginalPaper | Buchkapitel

Transient Mathematical Modeling and Simulation for an Open Cycle Liquid Rocket Engine

verfasst von : Taekyu Jung

Erschienen in: The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 2

Verlag: Springer Nature Singapore

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

This paper addresses the development and application of transient mathematical models and the in-house simulation code for the KRE-75 engine, which will be used as the 1st and 2nd stage engines of the Korea Space Launch Vehicle II. KRE-75 is the first Korean open-cycle liquid rocket engine that uses kerosene and liquid oxygen as propellants. Most of the components comprising the KRE-75 and the priming process of propellants in the propellant feed lines are considered. Startup and shutdown simulations of the KRE-75 are compared with engine ground test results and discussed in detail. The simulation results show good agreement with the test results, proving the validity of the transient mathematical models and the simulation code.

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Jetzt informieren

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Jetzt informieren
Vorheriges Kapitel Design and Verification of Turbofan Engine Clearance Measurement Based on High Energy X-ray
Nächstes Kapitel Effects of Grooved Pintle Tip Applied to a Gas–Liquid Pintle Injector
Literatur
1.
Kalnin VM, Sherstiannikov VA (1981) Hydrodynamic modelling of the starting process in liquid-propellant engines. Acta Astronaut 8:231–242CrossRef
2.
Martin MA, Nguyen HH, Greene WD et al (2003) Transient mathematical modeling for liquid rocket engine systems: Methods, capabilities, and experience. 5th International Symposium on Space Propulsion, Chattanooga, Tennessee, USA
3.
Liu K, Zhang Y (2000) A study on versatile simulation of liquid propellant rocket engine systems transients. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Huntsville, AL, USA, AIAA 2000-3771
4.
Ramesh D, Aminpoor M (2007) Nonlinear, dynamic simulation of an open cycle liquid rocket engine. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, DH, USA, AIAA 2007-5507
5.
Karimi H, Nassirharand A, Beheshti M (2003) Dynamic and nonlinear simulation of liquid-propellant engines. J Propul Power 19(5):938–944
6.
Ordonneau G, Albano G, Masse J (2002) CARINS: A future versatile and flexible tool for engine transient prediction. 4th International Conference on Launcher Technology “Space Launcher Liquid Propulsion”, Liege, Belgium
7.
Vaney R, Thomas V, Lekeux A (2002) Transient modelling of cryogenic rocket engines: A modular approach. 4th International Conference on Launcher Technology “Space Launcher Liquid Propulsion”, Liege, Belgium
8.
Durteste S (2007) A transient model of the VINCH cryogenic upper stage rocket engine. 43rd AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, DH, USA, AIAA 2007-5531
9.
Atsumi M, Ogawara A, Akazawa K, et al (2002) Development of visual integrated simulator for rocket engine cycle. 4th International Conference on Launcher Technology “Space Launcher Liquid Propulsion”, Liege, Belgium
10.
Kanumuri A, Wakamatsu Y, Shimura T, et al (1985) Start transient analysis of turbo pump-fed LOX/LH2 rocket engine (LE-5). National Aerospace Laboratory of Japan NAL-TR-868
11.
Lee S, Moon I (2015) Simulator development for startup analysis of staged combustion cycle engine power pack. J Kor Soc Propul Eng 19(5):62–70
12.
Lee S, Moon I (2016) Startup analysis of staged combustion cycle engine power pack. J Kor Soc Propul Eng 20(3):1–8
13.
Moon Y, Park S, Jung E (2016) Startup analysis of KSLV-II 75 tonf class liquid rocket engine. 2016 KSPE Spring Conference, Korea, pp 769–772
14.
Moon Y, Jung E (2016) A startup analysis of KSLV-II liquid rocket engine by ignition sequence of gas generator-combustion chamber. 2016 KSPE Fall Conference, Korea, pp 1010–1012
15.
Park S, Cho W, Moon Y (2011) Improvement of the startup transient analysis on the liquid rocket engine using the TP+GG coupled test result. 2011 KSPE Fall Conference, Korea, pp 821–826
16.
Jung T (2019) Development and evaluation of startup simulation code for an open cycle liquid rocket engine. J Kor Soc Propul Eng 23(5):67–74
17.
Jung T, Han S (2015) Pipe flow model for a liquid rocket engine startup analysis. 2015 SASE Spring Conference, Korea, pp 166–169
18.
Belyaev EN, Chvanov VK, Chervakov VV (1999) Mathematical modelling of liquid rocket engine. Moscow Aviation Institute Press, Moscow
19.
Jung T (2008) Combustion analysis program of liquid propellant rocket engine. Aero Eng Technol 7(2):163–167
20.
Kim S (2004) Non-equilibrium combustion modeling of extremely fuel-rich kerosene-LOx gas generators. KARI REG-TM-2004–007
21.
Gordon S, McBride B.J (1996) Computer program for calculation of complex chemical equilibrium compositions and applications. NASA RP-1311
22.
Moon Y, Nam C, Ha S et al (2017) Test requirement of 75 tonf liquid rocket engine 5g(QM). KARI L2-ES-01289
23.
24.
25.
Jung T, Lee S (2010) Development of BLDC motor driven cryogenic thrust control valve for liquid propellant rocket engine. Kor Soc Aero Space Sci 38(10):1026–1030
Metadaten
Titel
Transient Mathematical Modeling and Simulation for an Open Cycle Liquid Rocket Engine
verfasst von
Taekyu Jung
Copyright-Jahr
2023
Verlag
Springer Nature Singapore
Buch
The Proceedings of the 2021 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2021), Volume 2

Print ISBN: 978-981-19-2634-1

Electronic ISBN: 978-981-19-2635-8

Copyright-Jahr: 2023

DOI
https://doi.org/10.1007/978-981-19-2635-8_95

    Premium Partner

    Bildnachweise