Comparison of Solid Propellant Burning Rate Determination Methods from Industrial Point of View

Author(s):  
Özen Atak ◽  
Berkan Ziraman ◽  
Mine Yumusak
1999 ◽  
Vol 15 (6) ◽  
pp. 740-747 ◽  
Author(s):  
A. I. Atwood ◽  
T. L. Boggs ◽  
P. O. Curran ◽  
T. P. Parr ◽  
D. M. Hanson-Parr ◽  
...  

2009 ◽  
Author(s):  
To Kang ◽  
Hak-Joon Kim ◽  
Sung-Jin Song ◽  
Sun-Feel Ko ◽  
In-Chul Kim ◽  
...  

Marine Drugs ◽  
2018 ◽  
Vol 16 (10) ◽  
pp. 397 ◽  
Author(s):  
Isabel Viera ◽  
Antonio Pérez-Gálvez ◽  
María Roca

The benefit of carotenoids to human health is undeniable and consequently, their use for this purpose is growing rapidly. Additionally, the nutraceutical properties of carotenoids have attracted attention of the food industry, especially in a new market area, the ‘cosmeceuticals.’ Marine organisms (microalgae, seaweeds, animals, etc.) are a rich source of carotenoids, with optimal properties for industrial production and biotechnological manipulation. Consequently, several papers have reviewed the analysis, characterization, extraction and determination methods, biological functions and industrial applications. But, now, the bioaccessibility and bioactivity of marine carotenoids has not been focused of any review, although important achievements have been published. The specific and diverse characteristic of the marine matrix determines the bioavailability of carotenoids, some of them unique in the nature. Considering the importance of the bioavailability not just from the health and nutritional point of view but also to the food and pharmaceutical industry, we consider that the present review responds to an actual demand.


Author(s):  
V.A. Poryazov ◽  
◽  
K.M. Moiseeva ◽  
A.Yu. Krainov ◽  
◽  
...  

A problem of combustion of the composite solid propellants containing various powders of metals and non-metals is relevant in terms of studying the effect of various compositions of powders on the linear rate of propellant combustion. One of the lines of research is to determine the effect of the addition of a boron powder on the burning rate of a composite solid propellant. This work presents the results of numerical simulation of combustion of the composite solid propellant containing bidispersed boron powder. Physical and mathematical formulation of the problem is based on the approaches of the mechanics of two-phase reactive media. To determine the linear burning rate, the Hermance model of combustion of composite solid propellants is used, based on the assumption that the burning rate is determined by mass fluxes of the components outgoing from the propellant surface. The solution is performed numerically using the breakdown of an arbitrary discontinuity algorithm. The dependences of the linear burning rate of the composite solid propellant on the dispersion of the boron particles and gas pressure above the propellant surface are obtained. It is shown that the burning rate of the composite solid propellant with bidispersed boron powder changes in contrast to that of the composite solid propellant with monodispersed powder. This fact proves that the powder dispersion should be taken into account when solving the problems of combustion of the composite solid propellants containing reactive particles.


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