The objective was to prepare for the design of the space station propulsion system. Propulsion system concepts were defined and schematics were developed for the most viable concepts. A dual model bipropellant system was found to deliver the largest amount of payload. However, when resupply is considered, an electrolysis system with 10 percent accumulators requires less resupply propellant, though it is penalized by the amount of time required to fill the accumulators and the power requirements for the electrolyzer. A computer simulation was prepared, which was originally intended to simulate the water electrolysis propulsion system but which was expanded to model other types of systems such as cold gas, monopropellant and bipropellant storable systems.


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    Titel :

    Space Station Onboard Propulsion System: Technology Study


    Beteiligte:
    J. G. McAllister (Autor:in) / R. S. Rudland (Autor:in) / L. R. Redd (Autor:in) / D. H. Beekman (Autor:in) / S. M. Cuffin (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    106 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space station onboard propulsion system: Technology study

    Mcallister, J. G. / Rudland, R. S. / Redd, L. R. et al. | NTRS | 1987


    Space station propulsion system technology

    Jones, Robert E. / Meng, Phillip R. / Schneider, Steven J. et al. | NTRS | 1987


    Space Station propulsion system technology

    Jones, Robert E. / Meng, Phillip R. / Schneider, Steven J. et al. | Elsevier | 1987


    Space Station propulsion system technology

    Jones, Robert E. / Meng, Phillip R. / Schneider, Steven J. et al. | NTRS | 1987


    Space Station Propulsion System Technology

    R. E. Jones / P. R. Meng / S. J. Schneider et al. | NTIS | 1987