Significant component weight reductions are required to achieve the aggressive thrust-toweight goals for the Rocket Based Combined Cycle (RBCC) third-generation, reusable liquid propellant rocket engine, which is one possible engine for a future single-stage-toorbit vehicle. A collaboration between the NASA Glenn Research Center and Boeing Rocketdyne was formed under the Higher Operating Temperature Propulsion Components (HOTPC) program and, currently, the Ultra-Efficient Engine Technology (UEET) Project to develop carbon-fiber-reinforced high-temperature polymer matrix composites (HTPMCs). This program focused primarily on the combustor backup structure to replace all metallic support components with a much lighter polymer-matrixcomposite- (PMC-) titanium honeycomb sandwich structure.


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    Titel :

    High-Temperature Polymer Composites Tested for Hypersonic Rocket Combustor Backup Structure


    Beteiligte:


    Erscheinungsdatum :

    2005-06-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    High-Temperature Polymer Composites Tested for Hypersonic Rocket Combustor Backup Structure

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    3D rocket combustor acoustics model

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    Laser diagnostics on a hypersonic combustor

    TAYLOR, DAVID / OLDENBORG, R. / TIEE, J. et al. | AIAA | 1991