1986
DOI: 10.1016/0010-2180(86)90007-6
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Combustion of ammonium perchlorate-polymer sandwiches

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Cited by 122 publications
(56 citation statements)
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“…the protrsboundary of the crystal phase change layer sion is dramatic (10 MP*) 110, II, 151. The (240*C isotherm) in quenched samples 131, and with profiles calculated in a two-dimensional width and nature of the smooth band land model of the two-slab burning problem 1341. location of associated outer edge at region (4) 1 These results seem to establish unambiguously are relatively insensitive to pressure except to that heat flows from the AP to the binder over the extent that height of the region of AP the whale pressure rse. protrusion changes.…”
Section: E W Price Et Almentioning
confidence: 67%
See 1 more Smart Citation
“…the protrsboundary of the crystal phase change layer sion is dramatic (10 MP*) 110, II, 151. The (240*C isotherm) in quenched samples 131, and with profiles calculated in a two-dimensional width and nature of the smooth band land model of the two-slab burning problem 1341. location of associated outer edge at region (4) 1 These results seem to establish unambiguously are relatively insensitive to pressure except to that heat flows from the AP to the binder over the extent that height of the region of AP the whale pressure rse. protrusion changes.…”
Section: E W Price Et Almentioning
confidence: 67%
“…(9) and (12) The AP flame is present at all pressures down KLLEF standoff distance increases (row I -4) to 2 5 MPI or lower, and dominates the burning as pressure decreases (Eq. (12)1. and a correrate in the pressure range 10-14 MPa at all spondingly large portion of the fuel is consumed binder thicknesses, and at extremes of binder in the KLIEF at lower pressure (Eq (13) 1 thickness down to about 5 MPa (Fig. 5a,b).…”
Section: E W Price Et Almentioning
confidence: 98%
“…The burn rate, in SHORT COMMUNICATION turn depends upon particle characteristics of the oxidiser, metal fuel, and burn rate catalyst [3][4][5][6] . The coarse/fine combination of ammonium perchlorate affects the burn rate more prominently than the other ingredients used in composite propellants.…”
Section: Introductionmentioning
confidence: 99%
“…There are other additives in the propellant; but these are not considered at present. To understand the behaviour better, a two-dimensional analogue of the propellant has been experimentally investigated in the literature 19,20 . A schematic of this is shown in Fig.…”
Section: Combustion Of Composite Solid Propellantsmentioning
confidence: 99%