50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
DOI: 10.2514/6.2014-3884
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Combustion Characterization of Amine Borane Hypergolic Propellants

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Cited by 8 publications
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“…12 Although the density of TEAB is lower than that of MMH by 12%, the density-I sp (I sp ) of TEAB/WFNA is within 2% of MMH/RFNA because the stoichiometric oxidizer to fuel mass ratio is higher for TEAB. 11 Table 1 compares the performance of these propellant combinations. …”
Section: B Triethylamine Boranementioning
confidence: 99%
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“…12 Although the density of TEAB is lower than that of MMH by 12%, the density-I sp (I sp ) of TEAB/WFNA is within 2% of MMH/RFNA because the stoichiometric oxidizer to fuel mass ratio is higher for TEAB. 11 Table 1 compares the performance of these propellant combinations. …”
Section: B Triethylamine Boranementioning
confidence: 99%
“…They also showed that the combustion efficiency of TEAB/WFNA is nearly equivalent to MMH/RFNA with similar injection parameters in an impinging jet system. 11 According to the MSDS, liquid TEAB has a density of 777 kg/m 3 , a freezing point of -4°C, and a boiling point of 97°C. 12 Although the density of TEAB is lower than that of MMH by 12%, the density-I sp (I sp ) of TEAB/WFNA is within 2% of MMH/RFNA because the stoichiometric oxidizer to fuel mass ratio is higher for TEAB.…”
Section: B Triethylamine Boranementioning
confidence: 99%