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  • Spacecraft Design, Testing and Performance  (1)
  • 1995-1999  (1)
  • 1985-1989
  • 1
    Publikationsdatum: 2019-07-13
    Beschreibung: Current methods for defining the operational support requirements of new systems are data intensive and require significant design information. Methods are being developed to aid in the analysis process of defining support requirements for new launch vehicles during their conceptual design phase that work with the level of information available during this phase. These methods will provide support assessments based on the vehicle design and the operating scenarios. The results can be used both to define expected support requirements for new launch vehicle designs and to help evaluate the benefits of using new technologies. This paper describes the models, their current status, and provides examples of their use.
    Schlagwort(e): Spacecraft Design, Testing and Performance
    Materialart: AIAA Paper 95-3619 , AIAA 1995 Space Programs and Technologies Conference; Sep 26, 1995 - Sep 28, 1995; Huntsville, AL; United States
    Format: application/pdf
    Standort Signatur Erwartet Verfügbarkeit
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