The development of new launch vehicles will require that designers use innovative approaches to achieve greater performance in terms of pay load capability. The objective of the work performed under this delivery order was to provide technical assistance to the Contract Officer's Technical Representative (COTR) in the development of ideas and concepts for increasing the payload capability of launch vehicles by incorporating aerodynamic controls. Although aerodynamic controls, such as moveable fins, are currently used on relatively small missiles, the evolution of large launch vehicles has been moving away from aerodynamic control. The COTR reasoned that a closer investigation of the use of aerodynamic controls on large vehicles was warranted.


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    Titel :

    Aerodynamic Flight Control to Increase Payload Capability of Future Launch Vehicles


    Beteiligte:
    J. E. Cochran (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aerodynamic Flight Control to Increase Payload Capability of Future Launch Vehicles

    J. E. Cochran / Y. Cheng / T. Leleux et al. | NTIS | 1993


    Aerodynamic flight control to increase payload capability of future launch vehicles

    Cochran, John E., Jr. / Cheng, Y.-M. / Leleux, Todd et al. | NTRS | 1993


    Payload Requirements Data File for Future Launch Vehicles

    Rice, A. / Society of Logistics Engineers / AIAA | British Library Conference Proceedings | 1993