2016
DOI: 10.2514/1.b35591
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Solid Amine–Boranes as High-Performance and Hypergolic Hybrid Rocket Fuels

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Cited by 38 publications
(22 citation statements)
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“…52 The values obtained were then compared to those for paraffin fuels containing AB and aluminum for reference. AB in a paraffin matrix can yield hypergolic ignition, 14,19,34 just as our proposed use of HMOFs. Although aluminum particles as fuel additives do not yield hypergolicity, they were considered here for comparison as energetic rocket fuel additives.…”
Section: Theoretical Performancementioning
confidence: 90%
“…52 The values obtained were then compared to those for paraffin fuels containing AB and aluminum for reference. AB in a paraffin matrix can yield hypergolic ignition, 14,19,34 just as our proposed use of HMOFs. Although aluminum particles as fuel additives do not yield hypergolicity, they were considered here for comparison as energetic rocket fuel additives.…”
Section: Theoretical Performancementioning
confidence: 90%
“…To reduce the effects of varying particle size on ignition delay, the AB used for these initial tests was sieved into two particle size ranges: 45 < D < 150 μm, and D > 150 μm. These particle size ranges were selected to provide a comparison with previously published work by Pfeil et al [3]. To provide the most accurate comparison between the different synthesis methods, the primary focus of these initial tests was comparing the ammonia borane in the 45-150 μm particle size range.…”
Section: A Effects Of Synthesis Methods On Ignition Delaymentioning
confidence: 99%
“…For ammonia borane to be used in a conventional hybrid propellant system, it must first be mixed with a fuel binder to create a fuel grain with adequate mechanical properties. One of the major issues that has prevented further study of ammonia borane in solid and hybrid propellant formulations is that ammonia borane is incompatible with many of the fuel binders commonly used in propellant formulations [3]. Lee et al investigated using ammonia borane in a typical HTPB-AP composite propellant and found that adding ammonia borane to the propellant formulation resulted in the propellants failing to cure [13].…”
Section: Fuel Binder Compatibility Testingmentioning
confidence: 99%
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