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  <controlfield tag="008">260224s2009    xxu                      </controlfield>
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    <subfield code="a">Widegren, Jason A.</subfield>
    <subfield code="9">42270</subfield>
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    <subfield code="a">Bruno, Thomas J.</subfield>
    <subfield code="9">41674</subfield>
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    <subfield code="a">Thermal decomposition kinetics of kerosene-based rocket propellants. 2. RP-2 with three additives</subfield>
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    <subfield code="c">nov./dic. 2009</subfield>
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  <datafield tag="270" ind1=" " ind2=" ">
    <subfield code="a">08/06/2010 ; 08/06/2010</subfield>
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    <subfield code="a">5 p. ; 5523-5528</subfield>
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    <subfield code="a">Transcripci&#xF3;n del resumen del autor. The thermal decomposition of RP-2 with three potential stabilizing additives was investigated. The additives were 1,2,3,4-tetrahydroquinoline (THQ), 1,2,3,4-tetrahydronaphthalene (tetralin), and the additive package that is used to make JP-8 + 100 (herein referred to as the "+100 additive"). For mixtures of RP-2 with THQ and tetralin, the concentration of additive was 5% by mass. The mixture of RP-2 with the +100 additive contained only 256 mg/L of the additive (the same concentration used to make JP-8+100). Decomposition reactions were performed at 375, 400, 425, and 450 &#xB0;C in stainless steel reactors. At each temperature, the extent of decomposition as a function of time was determined by analyzing the thermally stressed liquid phase by gas chromatography. The results with each additive were compared to the decomposition of neat RP-2 under the same conditions. The addition of 5% THQ slowed the rate of decomposition by approximately an order of magnitude. The addition of 5% tetralin slowed the rate of decomposition by approximately 50%. At the low concentration tested, the +100 additive did not significantly change the thermal stability of the RP-2.</subfield>
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    <subfield code="a">BAAB</subfield>
    <subfield code="b">BAAB</subfield>
    <subfield code="d">2026-03-05</subfield>
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    <subfield code="r">2026-03-05 15:12:57</subfield>
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