The flight frequency of the Space Transportation System (STS) coupled with its large payload-carrying capability will provide an unprecedented opportunity for conducting aerothermodynamic/entry technology research. This STS research opportunity can be characterized into two distinct categories: (1) that research which will utilize the STS orbiter as the test vehicle, and (2) that research which will utilize a vehicle launched from the orbiter for entry. To date, on-going studies have defined experiments as well as the support systems required for the shuttle launched research program. The proposed Entry Technology Program will provide a flight data base from which accurate correlations can be performed relative to ground test and analysis data. These correlations will result in optimized designs for future flight systems.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Shuttle entry technology payloads


    Beteiligte:

    Kongress:

    Meeting on Space Shuttle Missions of the 80''s ; 1975 ; Denver, CO


    Erscheinungsdatum :

    1975-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Integrating Shuttle payloads

    Jean, O. C. / Lester, R. C. | NTRS | 1977


    Communication with Shuttle payloads

    Springett, J.C. / Udalov, S. | Tema Archiv | 1978


    Development of shuttle payloads

    Murphy, J. T. | NTRS | 1977


    1999 Shuttle Small Payloads Symposium

    Daelemans, Gerard / Mosier, Frances L. | NTRS | 1999