Four hypersonic research airplane configurations found to be the most cost effective were selected for further refinement. The selection was based on a systematic analysis and evaluation of realistic designs, involving nine different configurations, evolving from three different structural/thermal concepts, coupled with existing rocket and sustainer engines. All configurations were constrained by the mission profiles, research requirements, aerodynamic envelope and maximum launch weight established by NASA.


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    Titel :

    Configuration Development Study of the X-24C Hypersonic Research Airplane, Phase 1


    Beteiligte:
    H. G. Combs (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    368 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch