Experimental study on composite solid propellant material burning rate using algorithm MATLAB
In rocketry application, now-a-days instead of monopropellants slowly composite propellants are introduced. Burning rate of a solid state composite propellant depends on many factors like oxidizer-binder ratio, oxidizer particle size and distribution, particle size and its distribution, pressure,...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
VINCA Institute of Nuclear Sciences
2016-01-01
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Series: | Thermal Science |
Subjects: | |
Online Access: | http://www.doiserbia.nb.rs/img/doi/0354-9836/2016/0354-983616119T .pdf |
Summary: | In rocketry application, now-a-days instead of monopropellants slowly
composite propellants are introduced. Burning rate of a solid state composite
propellant depends on many factors like oxidizer-binder ratio, oxidizer
particle size and distribution, particle size and its distribution, pressure,
temperature, etc. Several researchers had taken the mass varied composite
propellant. In that, the ammonium perchlorate mainly varied from 85 to 90%.
This paper deals with the oxidizer rich propellant by allowing small
variation of fuel cum binder ranging from 2%, 4%, 6%, and 8% by mass. Since
the percent of the binder is very less compared to the oxidizer, the mixture
remains in a powder form. The powder samples are used to make a pressed
pellet. Experiments were conducted in closed window bomb set-up at pressures
of 2, 3.5, and 7 MN/m2. The burning rates are calculated from the combustion
photography (images) taken by a high-speed camera. These images were
processed frame by frame in MATLAB, detecting the edges in the images of the
frames. The burning rate is obtained as the slope of the linear fit from
MATLAB and observed that the burn rate increases with the mass variation of
constituents present in solid state composite propellant. The result
indicates a remarkable increase in burn rate of 26.66%, 20%, 16.66%, and
3.33% for Mix 1, 2, 3, 4 compared with Mix 5 at 7 MN/m2. The percentage
variations in burn rate between Mix 1 and Mix 5 at 2, 3.5, and 7 MN/m2 are
25.833%, 32.322%, and 26.185%, respectively. |
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ISSN: | 0354-9836 2334-7163 |