The Crew Exploration Vehicle (CEV) is required to maintain continuous abort capability from lift off through destination arrival. This requirement is driven by the desire to provide the capability to safely return the crew to Earth after failure scenarios during the various phases of the mission. This paper addresses abort trajectory design considerations, concept of operations and guidance algorithm prototypes for the portion of the ascent trajectory following nominal jettison of the Launch Abort System (LAS) until safe orbit insertion. Factors such as abort system performance, crew load limits, natural environments, crew recovery, and vehicle element disposal were investigated to determine how to achieve continuous vehicle abort capability.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Crew Exploration Vehicle Service Module Ascent Abort Coverage


    Beteiligte:
    M. B. Tedesco (Autor:in) / B. M. Eans (Autor:in) / D. S. Merritt (Autor:in) / R. D. Falck (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Crew Exploration Vehicle Service Module Ascent Abort Coverage

    Tedesco, Mark B. / Evans, Bryan M. / Merritt, Deborah S. et al. | NTRS | 2007


    Crew Exploration Vehicle Service Module Ascent Abort Coverage

    Tedesco, Mark / Evans, Bryan / Merritt, Deborah et al. | AIAA | 2007


    Crew Exploration Vehicle Service Module Ascent Abort Coverage AIAA Paper

    Tedesco, M. / Evans, B. / Merritt, D. et al. | British Library Conference Proceedings | 2007


    Crew Exploration Vehicle Ascent Abort Coverage Analysis

    Abadie, Marc J. / Berndt, Jon S. / Burke, Laura M. et al. | NTRS | 2007


    Crew Exploration Vehicle Ascent Abort Overview

    Davidson, John B., Jr. / Madsen, Jennifer M. / Proud, Ryan W. et al. | NTRS | 2007