OVERVIEW For every pound of payload landed on Mars, 226 pounds are required on Earth to get it there. Due to this enormous mass gear‐ratio, increasing commonality between lander subsystems, such as power, propulsion, and life support, results in tremendous launch mass and cost savings. Human‐Mars architectures point to an oxygen‐methane economy, utilizing common commodities scavenged from the planetary atmosphere and soil via In‐Situ Resource Utilization (ISRU) and common commodity tankage across sub‐systems.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    LOx/LCH4: A Unifying Technology for Future Exploration


    Beteiligte:
    Banker, Brian (Autor:in) / Ryan, Abigail (Autor:in)

    Kongress:

    JSC OCT (Office of the Chief Technologist) Technology Poster Session ; 2014 ; Houston, TX, United States


    Erscheinungsdatum :

    18.11.2014


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    LOx / LCH4: A Unifying Technology for Future Exploration

    Falker, John / Terrier, Douglas / Clayton, Ronald G. et al. | NTRS | 2015


    Design and Development of a LOX/LCH4 Technology Demonstrator

    Salvatore, Vito / Battista, Francesco / Votta, Raffaele et al. | AIAA | 2012


    100-LBF LO2/LCH4 - Reaction Control Engine Technology Development for Future Space Vehicles

    Robinson, Philip J. / Veith, Eric M. / Hurlbert, Eric A. et al. | NTRS | 2008



    100-Lb(f) LO2/LCH4 Reaction Control Engine Technology Development for Future Space Vehicles

    Robinson, Philip J. / Veith, Eric M. / Hurlbert, Eric A. et al. | NTRS | 2008