Beginning in 2006, NASA initiated the J-2X engine development effort to develop an upper stage propulsion system to enable the achievement of the primary objectives of the Constellation program (CxP): provide continued access to the International Space Station following the retirement of the Space Station and return humans to the moon. The J-2X system requirements identified to accomplish this were very challenging and the time expended over the five years following the beginning of the J- 2X effort have been noteworthy in the development of innovations in both the fields for liquid rocket propulsion and system engineering.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    System Engineering and Technical Challenges Overcome in the J-2X Rocket Engine Development Project


    Beteiligte:

    Kongress:

    4th European Conference for Aerospace Sciences (EUCASS) ; 2011 ; Saint Petersburg, Russia


    Erscheinungsdatum :

    04.07.2012


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Liquid rocket engine test facility engineering challenges

    Ellerbrock, Hartwig | Online Contents | 2006


    Technical Challenges for Next Generation Liquid Rocket Engine Nozzles

    Clinton, R. G., Jr. / Eckel, Andy / Self, Kennt et al. | NTRS | 1998


    Rocket engine development

    Engineering Index Backfile | 1965


    Rocket engine development.

    Butler, Kathleen N. | Online Contents | 1993