Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings

Timothy P. Kibbey, Andrew C. Cortopassi, J. Eric Boyer

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    2 Citations (Scopus)

    Abstract

    A design of experiments was conducted to explore the regression rate performance of aluminized hybrid rocket fuels in gaseous oxygen. Mass flux, pressure, diameter, and aluminum content were varied independently in a 2-level, full factorial, 16-run experiment design. The least important 4 tests were run first so that any adjustments could be made as the device became better characterized with this setup and these propellants. This resulted in an effective set of data over orthogonal parameter spaces that led to a model depending on the mass flux, the diameter, and the aluminum loading, while showing pressure to be of no effect.

    Original languageEnglish (US)
    Title of host publication53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
    PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN (Print)9781624105111
    StatePublished - Jan 1 2017
    Event53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 - Atlanta, Georgia
    Duration: Jul 10 2017Jul 12 2017

    Other

    Other53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
    CountryGeorgia
    CityAtlanta
    Period7/10/177/12/17

    Fingerprint

    Mass transfer
    Aluminum
    Propellants
    Rockets
    Design of experiments
    Oxygen
    Experiments

    All Science Journal Classification (ASJC) codes

    • Engineering(all)

    Cite this

    Kibbey, T. P., Cortopassi, A. C., & Boyer, J. E. (2017). Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings. In 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 American Institute of Aeronautics and Astronautics Inc, AIAA.
    Kibbey, Timothy P. ; Cortopassi, Andrew C. ; Boyer, J. Eric. / Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017.
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    abstract = "A design of experiments was conducted to explore the regression rate performance of aluminized hybrid rocket fuels in gaseous oxygen. Mass flux, pressure, diameter, and aluminum content were varied independently in a 2-level, full factorial, 16-run experiment design. The least important 4 tests were run first so that any adjustments could be made as the device became better characterized with this setup and these propellants. This resulted in an effective set of data over orthogonal parameter spaces that led to a model depending on the mass flux, the diameter, and the aluminum loading, while showing pressure to be of no effect.",
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    year = "2017",
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    Kibbey, TP, Cortopassi, AC & Boyer, JE 2017, Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings. in 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017, Atlanta, Georgia, 7/10/17.

    Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings. / Kibbey, Timothy P.; Cortopassi, Andrew C.; Boyer, J. Eric.

    53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

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    N2 - A design of experiments was conducted to explore the regression rate performance of aluminized hybrid rocket fuels in gaseous oxygen. Mass flux, pressure, diameter, and aluminum content were varied independently in a 2-level, full factorial, 16-run experiment design. The least important 4 tests were run first so that any adjustments could be made as the device became better characterized with this setup and these propellants. This resulted in an effective set of data over orthogonal parameter spaces that led to a model depending on the mass flux, the diameter, and the aluminum loading, while showing pressure to be of no effect.

    AB - A design of experiments was conducted to explore the regression rate performance of aluminized hybrid rocket fuels in gaseous oxygen. Mass flux, pressure, diameter, and aluminum content were varied independently in a 2-level, full factorial, 16-run experiment design. The least important 4 tests were run first so that any adjustments could be made as the device became better characterized with this setup and these propellants. This resulted in an effective set of data over orthogonal parameter spaces that led to a model depending on the mass flux, the diameter, and the aluminum loading, while showing pressure to be of no effect.

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    Kibbey TP, Cortopassi AC, Boyer JE. Characterization and detailed analysis of regression behavior for HTPB solid fuels containing high aluminum loadings. In 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA. 2017