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Titles and Abstracts for Issue 22, Winter 2005
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Interior
Pressure in the Mortar and Motion of a No. 3 Shell in a Fireworks
Shot |
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Yuzo Ooki, Dayu Ding, Masamori Higaki and
Tadao Yoshida Department of Mechanical
Engineering, Ashikaga Institute of Technology, 268-Omae-cho, Ashikaga-shi,
Tochigi 326-8558, Japan |
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Abstract: Interior pressure
in a fireworks mortar and initial velocity for the shot of a no.
3 shell were measured and results were analyzed. The observed initial
velocity was mainly explained by the action of the interior pressure
during the shot. On the other hand, a delay in pressure propagation
in the mortar, the effect of gas flow through the gap between the
mortar and shell, and acceleration of the shell just after leaving
the muzzle were suggested.
Keywords: fireworks, shot,
interior ballistics, initial velocity
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A Prediction of Aerial Shell and Comet
Trajectories Using SHELLCALC© |
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John Harradine and Tom Smith
Manly, Queensland, Australia; Davas
Ltd, 8 Aragon Place, Kimbolton, UK |
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Abstract: This paper describes
a model for predicting the path of aerial shells and Roman candle
comets. This model, incorporated in a Microsoft® Excel-based freeware
program, SHELLCALC©, predicts the trajectory of these fireworks
using point mass equations for range and height. These equations
are modified to take into consideration mortar/candle angle, launch
altitude above sea level, wind speed and direction, comet consumption,
air density and terrain, and incorporate an approximation of shell
drift through tumbling motion and mortar balloting. The graphical
output from the model also incorporates typical shell burst diameters.
Keywords: shells, comets,
ballistics, trajectory, fall-out
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Reaction
propagation between fireworks shells and compositions confined in
steel pipes |
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E. Contestabile and B. von Rosen
Canadian Explosive Research Lab, 555 Booth St., Ottawa, Ontario K1A
0G1, Canada |
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Abstract: This study presents
the experimental results on the ignition of linear arrays of fireworks
articles and bulk stars and describes their propensity to mass explode.
Star and report shells, roman candles, and bulk cylindrical and
spherical stars were functioned in steel pipes through initiation
with a small black powder charge or an explosives booster. Continuous
velocity of detonation probes was used to monitor the rate of reaction
among the pyrotechnic components and the resultant fragmentation
of the steel pipe was used to rate the violence of the reaction.
All pipes fragmented and the measured reaction rate ranged from
170 to 870 ms-1. Based on fragmentation, the violence
of reaction increased from the star shells, to the roman candles,
to the report shells, and then to the bulk stars.
Keywords: explosion, steel,
mortars, fragments, reports
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Thermodynamic
and Spectroscopic Analysis of a Simple Lilac Flame Composition |
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B. T. Sturman and K. L. Kosanke
6 Corowa Court, Mount Waverley, Victoria 31 49, Australia;
PyroLabs, Inc., Whitewater, CO, USA |
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Abstract: A simple lilac flame
composition consisting of 80% potassium nitrate and 20% shellac
was investigated by emission spectroscopy and thermodynamic modeling.
The flame from the burning composition had a reddish-pink core with
a brighter pale lilac outer envelope. The core of the flame is presumably
close to the equilibrium conditions predicted by thermodynamic modeling.
The calculated equilibrium flame temperature is 1526 K; seven gases
(CO, H2O, N2, CO2, H2,
KOH, K) and one liquid (K2CO3) account for
99.7% of the molecules in the core of the flame. Of these, liquid
potassium carbonate (mole fraction 9.6%) is expected to emit a continuous
spectrum while atomic potassium (mole fraction 2.5%) imparts a red
colour from the resonance doublet (766.491 and 769.897 nm), which
is considerably broadened by self-absorption. The outer flame envelope
is presumably a diffusion flame in which flammable gases from the
core burn in entrained air. The maximum adiabatic temperature of
such a flame was calculated as 1723 K; seven gases (N2,
CO2, H2O, KOH, K, Ar, K2O2H2)
account for 99.8% of the molecules in the outer flame envelope.
The emission spectrum of atomic potassium superimposed on a continuous
spectrum arising from the combining of atomic potassium with OH
radicals to form gaseous KOH is responsible for the lilac colour
of laboratory flames containing potassium and is the likely cause
of the lilac colour of the outer regions of this pyrotechnic flame.
The article includes a brief tutorial outline of some relevant aspects
of the atomic spectroscopy of potassium.
Keywords: lilac flame colour,
potassium nitrate, shellac, thermodynamic modeling, visible spectrum
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A
Thrust and Impulse Study of Guanidinium Azo-Tetrazolateas a Fuel
Additive for Hybrid Rocket Motor |
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Ann Wrighta, Warfield Teaguea,
M. Keith Hudsonb, Andrew Wrightb, Patrick Foleyb
aDepartment of Physics and Department of Chemistry, Hendrix
College, Conway, AR 72032, USA;
bDepartment of Applied Science and the Graduate Institute
of TechnologyUniversity of Arkansas at Little Rock, Little Rock, AR
72204, USA |
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Abstract: Guanidinium azo-tetrazolate
(GAT) is an organic salt with a high percentage of nitrogen. GAT was
mixed with the standard hybrid rocket fuel, hydroxyl-terminated polybutadiene
(HTPB), in concentrations of 15% and 25% by mass. The fuel grains
with the GAT additive were fired for 4 seconds with oxygen flows of
0.04, 0.06, 0.08, and 0.10 lbm/sec. Physical characteristics of the
rocket were measured while firing the GAT fuels. Thrust, internal
pressure, fuel mass consumed, oxygen flow rate, nozzle throat diameter,
and fuel port radius were measured. Fuel regression rate, specific
impulse, total impulse, and average thrust were calculated from the
data.
GAT was found to increase the thrust output when added to the standard
hybrid rocket fuel, HTPB. 25% GAT fuel produced approximately the
same thrust as the 15% GAT fuel. Specific impulse was slightly lower
with both 15% and 25% GAT fuels than with plain HTPB fuel.Standard
deviation of thrust was used as a crude measure of amplitude of
oscillations during combustion. GAT-added fuels showed a very small
decrease in thrust oscillation amplitude.
Keywords: GAT, rocket, additive,
motor
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Pressure
in a Mortar and Estimation of Muzzle Velocity of Expelled Stars
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Dayu Ding, Morimasa Higaki, Yuzo Ooki,
and Tadao Yoshida Ashikaga Institute
of Technology268-1 Omae-cho, Ashikaga-shi, Tochigi 326-8558, Japan |
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Abstract: Firing firework star
experiments have been carried out using 20 mm and 25 mm inner diameter
steel mortars equipped with two or four pressure transducers, and
the pressure profiles were recorded. The relative pressure profiles
of the four positions in the mortar changed with the gap ratio between
sectional areas of the star and the mortar wall, and with the mass
of the lifting charge. The maximum pressure attained decreased and
the scatter of observed data increased with an increase of the gap
ratio. It was shown by experiment using four pressure transducers
that, when the gap ratio is large, the pressures to the rear and front
of a star should be corrected for the pressure distribution in the
mortar. In the first half of the experiment, using two pressure
transducers the muzzle velocity of a star was estimated from the
pressure profile of the bottom transducer. When the gap between
star and mortar wall and the mass of lifting charge were small,
the calculated and observed muzzle velocities agreed well. However,
in the case of a large gap, the calculated value was larger than
the observed one.
In the latter half of the experiment, four pressure transducers
were used and it was found that in the case of a large gap the pressure
profile from the bottom transducer did not give the real pressures
to the rear and front of the star in the mortar. A correction for
the difference was tried and the agreement between the observed
and calculated values was improved.
Keywords: fireworks, interior
ballistics, pressure profile, muzzle velocity
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Notes
on chlorinated rubber and some other chlorine donors |
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Barry T. Sturman
6 Corowa Court, Mount Waverley, Victoria 31 49, Australia |
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Abstract: A brief review is
given of the history and technology of chlorinated rubber. The empirical
formula is approximately (C10H11C17)n,
corresponding to 65.4% Cl. The structure is complex, and includes
partially chlorinated cyclohexane rings. All the Cl is released
as HCl on pyrolysis. The enthalpy of formation was estimated from
the reported heat of combustion as -395 kJ/mol. For comparison,
the enthalpy of formation of solid polyvinyl chloride (C2H3Cl)n
was reported to be -94.6 kJ/mol and that of solid polyvinylidene
chloride (C2H2Cl2)n
was reported to be -100.4 kJ/mol.
Keywords: chlorinated rubber,
Parlon, enthalpy of formation, chlorine donors, PVC, polyvinyl chloride,
polyvinylidene chloride
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Communications
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An Introduction to the European CHAF Project by D. Chapman
Abstract: The CHAF project was
instigated following a series of accidents in large-scale storage
of fireworks, by far the most serious being that at Enschede in
the Netherlands. The project aims to quantify and suggest means
to control the hazards associated with large-scale fireworks storage
by small-, medium- and large-scale investigations on a series of
well-defined fireworks. Additionally, it is hoped that correlations
will be found between the small- and/or medium-scale tests results
and those obtained in large-scale trials, and that these will lead
to better test methods to predict mass storage hazards. Reports
from the individual activities undertaken in the workpackages are
posted on a dedicated web site www.chaf.info as they are delivered.
Review by Tom Smith of: Review
of Firework Art by Mark Flemming
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