The propellant management of the precooled turbojet engine

Akiko Hasegawa, Katsuyoshi Otsuka, Hitomi Lizuka, Masamitsu Watanabe, Tetsuya Satou, Hiroaki Kobayashi, Hideyuki Taguchi

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Abstract

    This paper shows the LH2 propellant management of the precooled turbo jet engine "PCTJ". On the fuel supply system of the core-engine, liquid hydrogen is vaporized in the evaporator in the combustor and supplied to the combustor. The hydrogen changes its density drastically with accompanying its phase (liquid, gaseous and two-phase flow) depending on time and space. Hence, it is very difficult to control the mass flow rate especially at the start-up transient condition. In this study, the transient variation of the hydrogen flow rate is simulated by using the heat transfer model which includes several boiling styles. The result has a quantitative difference from the experimental data though the trend is similar. Thus, a test on the boiling heat transfer of liquid hydrogen is planed to get the heat transfer and pressure loss data for improvement of the simulation accuracy. The heat transfer depends on the boiling style and void fraction. In advance of the hydrogen test, preliminary test using deionized water and air was conducted to construct the method of void fraction measurement using the capacitance meter and high-speed camera.

    Original languageEnglish
    Title of host publication60th International Astronautical Congress 2009, IAC 2009
    Pages6442-6450
    Number of pages9
    Volume8
    Publication statusPublished - 2009
    Event60th International Astronautical Congress 2009, IAC 2009 - Daejeon
    Duration: 2009 Oct 122009 Oct 16

    Other

    Other60th International Astronautical Congress 2009, IAC 2009
    CityDaejeon
    Period09/10/1209/10/16

    Fingerprint

    turbojet engines
    propellants
    engine
    heat transfer
    hydrogen
    boiling
    liquid hydrogen
    combustion chambers
    voids
    void
    liquid
    jet engines
    evaporators
    high speed cameras
    mass flow rate
    two phase flow
    engines
    liquid phases
    flow velocity
    capacitance

    ASJC Scopus subject areas

    • Space and Planetary Science
    • Astronomy and Astrophysics

    Cite this

    Hasegawa, A., Otsuka, K., Lizuka, H., Watanabe, M., Satou, T., Kobayashi, H., & Taguchi, H. (2009). The propellant management of the precooled turbojet engine. In 60th International Astronautical Congress 2009, IAC 2009 (Vol. 8, pp. 6442-6450)

    The propellant management of the precooled turbojet engine. / Hasegawa, Akiko; Otsuka, Katsuyoshi; Lizuka, Hitomi; Watanabe, Masamitsu; Satou, Tetsuya; Kobayashi, Hiroaki; Taguchi, Hideyuki.

    60th International Astronautical Congress 2009, IAC 2009. Vol. 8 2009. p. 6442-6450.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Hasegawa, A, Otsuka, K, Lizuka, H, Watanabe, M, Satou, T, Kobayashi, H & Taguchi, H 2009, The propellant management of the precooled turbojet engine. in 60th International Astronautical Congress 2009, IAC 2009. vol. 8, pp. 6442-6450, 60th International Astronautical Congress 2009, IAC 2009, Daejeon, 09/10/12.
    Hasegawa A, Otsuka K, Lizuka H, Watanabe M, Satou T, Kobayashi H et al. The propellant management of the precooled turbojet engine. In 60th International Astronautical Congress 2009, IAC 2009. Vol. 8. 2009. p. 6442-6450
    Hasegawa, Akiko ; Otsuka, Katsuyoshi ; Lizuka, Hitomi ; Watanabe, Masamitsu ; Satou, Tetsuya ; Kobayashi, Hiroaki ; Taguchi, Hideyuki. / The propellant management of the precooled turbojet engine. 60th International Astronautical Congress 2009, IAC 2009. Vol. 8 2009. pp. 6442-6450
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