Potential collision or accidental recontact problems between the spacecraft and other space vehicles (or components) existed during most of the Apollo missions. These problems were identified before each Apollo flight, and appropriate solutions for eliminating or minimizing the chance of collision were determined through relative motion analyses. A summary of the identification, solution, and analysis process for some of the more significant of these separation problems is presented. In addition, the scope of responsibility, the development of the study effort, and the computer simulation development, which supported the analysis process, are described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Apollo experience report: Spacecraft relative motion and recontact analyses


    Beteiligte:
    Mcadams, R. E. (Autor:in) / Gott, C. J. (Autor:in) / Williamson, M. L. (Autor:in)

    Erscheinungsdatum :

    01.04.1975


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Apollo Experience Report: Spacecraft Relative Motion and Recontact Analyses

    R. E. Mcadams / C. J. Gott / M. L. Williamson | NTIS | 1975


    Apollo experience report ; [92]: Spacecraft relative motion and recontact analyses

    MacAdams, Robert E. / Gott, Charles J. / Williamson, Marland L. | TIBKAT | 1975



    Contamination of spacecraft by recontact of dumped liquids

    Fowler, M. E. / Leger, L. J. / Donahoo, M. E. et al. | NTRS | 1990


    Capsule Abort Recontact Simulation

    Pandya, Shishir / Onufer, Jeffrey / Chan, William et al. | AIAA | 2006