A pressure-fed hypergolic bi-propellant system is the assumed propulsion approach for the Reaction Control System (RCS) used by the Mars Transit Habitat (TH), an architectural concept being traded within the NASA Moon to Mars architecture. The propellants under consideration are Monomethyl Hydrazine (MMH) and Mixed Oxides of Nitrogen with 3% Nitric Oxide (MON3), with helium pressurant.


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    Titel :

    Propulsion System Architecture Refueling Capability Assessment for A Mars Transit Habitat Concept


    Beteiligte:
    H. P. Trinh (Autor:in) / C. G. Popp (Autor:in) / B. M. Addona (Autor:in) / C. W. Pierce (Autor:in)

    Erscheinungsdatum :

    2024


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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