Three candidate hybrid propulsion (HP) concepts were identified, optimized, evaluated, and refined through an iterative process that continually forced improvement to the systems with respect to safety, reliability, cost, and performance criteria. A full scale booster meeting Advanced Solid Rocket Motor (ASRM) thrust-time constraints and a booster application for 1/4 ASRM thrust were evaluated. Trade studies and analyses were performed for each of the motor elements related to SRM technology. Based on trade study results, the optimum HP concept for both full and quarter sized systems was defined. The three candidate hybrid concepts evaluated are illustrated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hybrid Propulsion Technology Program: Phase 1. Volume 3: Thiokol Corporation Space Operations


    Beteiligte:
    A. L. Schuler (Autor:in) / D. R. Wiley (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    99 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Thiokol Corporation-Space Operations Fastener Controls

    Dye, K. / National Aeronautics and Space Administration | British Library Conference Proceedings | 1995