28th Joint Propulsion Conference and Exhibit 1992
DOI: 10.2514/6.1992-3049
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Particle size distribution measurements in a subscale motor for the Ariane 5 solid rocket booster

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Cited by 7 publications
(9 citation statements)
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“…At the nozzle exit the particle mean size remained in the lower limit size range (submicron to micron) of the diagnostic device (Malvern 2600 HSD with a 100-mm range lens). The mass fraction of particles smaller than 2 jit at the nozzle exit was found to be 8-35% for pressures greater than 3.2 MPa, in some contrast to other reported results 6 where the mass fractions were less than 10%. It should be noted that the particle breakup requires not only the attainment of a critical Weber number but also time at this condition.…”
Section: Particle Size Distributions Propellant To Plumecontrasting
confidence: 82%
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“…At the nozzle exit the particle mean size remained in the lower limit size range (submicron to micron) of the diagnostic device (Malvern 2600 HSD with a 100-mm range lens). The mass fraction of particles smaller than 2 jit at the nozzle exit was found to be 8-35% for pressures greater than 3.2 MPa, in some contrast to other reported results 6 where the mass fractions were less than 10%. It should be noted that the particle breakup requires not only the attainment of a critical Weber number but also time at this condition.…”
Section: Particle Size Distributions Propellant To Plumecontrasting
confidence: 82%
“…Those results ( Table 2) had a higher mass percentage of <2-ju particles (approximately 9 vs Q.2%) and a smaller maximum particle size (12 vs 84 jn). Traineau et al 6 reported (for a different propellant and operating conditions) approximately 10% of the mass in particle with diameters <2 /A, most particles smaller than 75 /x, and a maximum diameter of 120 ju. Although these results for the nozzle entrance vary somewhat for the different propellants and test conditions, they give a consistent picture.…”
Section: Comparison With Other Datamentioning
confidence: 98%
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