John C. Stennis Space Center (SSC) provides rocket engine propulsion testing for NASA's space programs. Since the development of the Space Shuttle, every Space Shuttle Main Engine (SSME) has undergone acceptance testing at SSC before going to Kennedy Space Center (KSC) for integration into the Space Shuttle. The SSME is a large cryogenic rocket engine that uses Liquid Hydrogen (LH2) as the fuel. As NASA moves to the new ARES V launch system, the main engines on the new vehicle, as well as the upper stage engine, are currently base lined to be cryogenic rocket engines that will also use LH2. The main rocket engines for the ARES V will be larger than the SSME, while the upper stage engine will be approximately half that size. As a result, significant quantities of hydrogen will be required during the development, testing, and operation of these rocket engines.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hydrogen Reclamation and Reutilization


    Contributors:
    B. Hebert (author) / J. Lansaw (author)

    Publication date :

    2009


    Size :

    3 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Hydrogen Reclamation and Reutilization

    Hebert, Bartt / Lansaw, John | NTRS | 2009


    WING ENERGY REUTILIZATION SYSTEM

    ELGHAZALI AHMED FAWZI ABDULMOATI ABDELLATIF | European Patent Office | 2024

    Free access

    Wing energy reutilization system

    ELGHAZALI AHMED FAWZI ABDULMOATI ABDELLATIF | European Patent Office | 2025

    Free access

    River water ecological management and reutilization system

    YANG DESHENG / SONG CE / ZHAO WENMING et al. | European Patent Office | 2020

    Free access

    The Technologies Concerning Reutilization of Plastic Materials

    Toh, K. / Sasaki, K. | British Library Online Contents | 1997