1976
DOI: 10.2514/3.7167
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Radiative ignition of double-base propellants. I - Some formulation effects

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Cited by 86 publications
(24 citation statements)
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“…Depending on the mode of peat ignition (smoldering or flaming), the ignition time was determined by the yes/no criterion [11] or the occurrence of flame. In this work, in contrast to the yes/no criterion from [11], as the ignition time we used the minimum exposure time of the radiation flux that led to the development of combustion in at least one case; i.e., after the cessation of irradiation, the sample was observed for 20 min, and if peat combustion continued, it was considered that peat ignition occurred.…”
Section: Methodsmentioning
confidence: 99%
“…Depending on the mode of peat ignition (smoldering or flaming), the ignition time was determined by the yes/no criterion [11] or the occurrence of flame. In this work, in contrast to the yes/no criterion from [11], as the ignition time we used the minimum exposure time of the radiation flux that led to the development of combustion in at least one case; i.e., after the cessation of irradiation, the sample was observed for 20 min, and if peat combustion continued, it was considered that peat ignition occurred.…”
Section: Methodsmentioning
confidence: 99%
“…No criterion whatsoever is found in the literature for the case of dynamic extinction by fast deradiation reported by the Princeton group (Refs. [38][39][40]. As to the low pressure extinction (or PDL extinction), a large amount of experimental and theoretical work was performed on pure AP deflagration but without conclusive results; less work appears to have been done on AP-based composite propellants and even less on other propellants.…”
Section: -Plan Of Presentation Of This Reportmentioning
confidence: 99%
“…This line of research was motivated by experimental results, on dynamic extinction by fast deradiation collected by the senior author during his stay at Princeton University (Refs. 12,[38][39][40]. An original theoretical approach of nonlinear burning stability of solid propellants was hence developed (Refs.…”
Section: -3mentioning
confidence: 99%
“…(ii) §ame retention, or the ability of the propellant to self-sustain upon removal of the external heat §ux; and (iii) §ame spreading, or the ability for propellant adjacent to the ignition site to become ignited [3].…”
Section: Introductionmentioning
confidence: 99%