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  • 1
    Publication Date: 2019-06-28
    Description: Consideration is given to two methods developed for the evaluation, screening, and ranking of concepts for Space Exploration Initiative vehicle propellant management systems. The methods selected for handling this multicriteria decision problem are based on the utility theory which transforms both qualitative and quantitative criteria into a nondimensional utility scale for comparison of dissimilar figures of merit. The development of the resultant FSA evaluation criteria and concept evaluation methodology is summarized.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: AIAA PAPER 91-3479
    Format: text
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  • 2
    Publication Date: 2019-06-28
    Description: Specific propellant management system requirements have been identified for each facility category of SSF. Distributed systems have been analyzed to indentify momentum management, guidance, and traffic management requirements associated with the guidance, navigation, and control system; space-to-space communications and enhanced tracking requirements associated with the communications and tracking system; and propellant management system utility requirements associated with the electrical power system. Flight element analyses determined attach structure, utility distribution, and structural integrity requirements for the pre-integrated truss and high mass manipulation and translation requirements for the mobile base system.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: AIAA PAPER 91-3476
    Format: text
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