The factors that significantly affect the operability of aerospace planes are identified and considered in terms of the development of the National Aerospace Plane (NASP). The aircraftlike vehicle can be affected by variables related to the structure, propulsion, and mechanical elements of the design. The requirements to control the factors are listed including robustness, fuels and propellants, maintainability, autonomy, and development testing. The details of the requirements indicate critical factors such as the strength-to-weight ratios of the materials, propellant-system components that can withstand 5000 consecutive cycles, and low vehicle-failure probabilities. The NASP program is concluded to require: (1) models for quantitative operational assessments; (2) a modular design for the NASP structure; (3) computer-technology integration; and (4) technologies to support and normalize cryogenic operations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Operational design factors for NASP derived vehicles


    Beteiligte:
    Hickman, R. A. (Autor:in) / Adams, J. D. (Autor:in)

    Erscheinungsdatum :

    01.12.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Operational design factors for NASP derived vehicles

    HICKMAN, R. / ADAMS, J. | AIAA | 1991


    NASP derived vehicles - Not just to space

    JOHNSON, DONALD / ESPINOSA, ANGEL / ALTHUIS, JEFFREY | AIAA | 1992


    Information Requirements Analysis for NASP-derived vehicles

    KUPERMAN, GILBERT / SOBEL, ANNETTE | AIAA | 1992


    NASP aerodynamics

    Whitehead, Allen H., Jr. | NTRS | 1989


    CFD support of NASP design

    MCCLINTON, CHARLES / BITTNER, ROBERT / KAMATH, PRADEEP | AIAA | 1990