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Titles and Abstracts for Issue 20, Winter 2004
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Simple
Core Design for Neutral Burn Composite Rocket Motors |
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S. K. Anderson 13528
Elsie Road, Conifer, CO 80433, USA |
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Abstract: Two simple techniques
for improving small amateur style rocket motors are discussed. The
first uses a simple, post-cure technique to produce neutral thrust
profiles using a simple machinist’s tap. The second uses a small
Black Powder pellet to improve reliability and ignition of composite
rocket motors.
Keywords: rocket motor, composite
propellant, thrust profile, neutral burn, neutral thrust characteristic
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Clive Jennings-White 3096
S. 2300 E., Salt Lake City, Utah 84109, USA |
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Abstract: Pyrotechnic strobe
compositions burn in an oscillatory manner such that there is a
marked variation of emitted light intensity as a function of time.
The most common theoretical explanation for the phenomenon is that
such compositions contain within them sub-compositions that may
be regarded as a smoulder composition and a flash composition. The
smoulder reaction would have a lower activation energy and low heat
output. The flash reaction would have a high activation energy and
high heat output. The actual chemical components of strobe compositions
are extremely diverse, confounding a unified chemistry of the phenomenon.
Nevertheless the majority of strobe compositions can in fact be
reasonably deconstructed into smoulder and flash compositions. However,
there appear to be a few strobe compositions that defy such explanation;
although it is possible that the author lacks the wit to comprehend
the chemistry. It is also possible that the prevailing theory applies
to some, but not to all, strobe compositions; and it is yet possible
that a different theory will provide a more encompassing explanation
with better predictive power.
Keywords: strobe, formulation,
theory, flash, magnalium, smoulder, smolder
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Maximizing
the Number of Electric Matches That Can Be Fired in a Single Circuit |
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Michael A. Tockstein Pyrotechnic
Innovations, Wilmington, CA 90744 USA |
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Abstract: For a given electric
match resistance and wire gauge, the number of electric matches
that one can fire in a single circuit, using a standard DC firing
system, depends on the arrangement in which the electric matches
are wired (series, parallel or series-parallel). The number of electric
matches fired from a single cue can be maximized by utilizing series-parallel
circuits. This is demonstrated using graphs of the amount of current
that is sent through each electric match in various series and parallel
combinations. This data allows one to determine the maximum number
of electric matches that can be successfully fired in a single circuit.
Keywords: electric match, all
fire current, cue, electrical firing, resistance
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Sparking
Compositions for Garden Fireworks |
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A. V. Belyakov, A. I. Khatsrinov,
G. S. Baturova, L. A. Kiprova, E. N. Panferova
Department of Chemistry and Technology of Heterogeneous Systems, Kazan'
State Technological University, Kazan', Russia |
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Abstract: As a result of studies
performed, the burn rate and characteristics of the special effect
of sparking compositions are established. A method of determining
the spark characteristics by photographic method is tested. The
results from improvement in the formulation of compositions for
components used in garden fireworks are presented.
Keywords: garden fireworks,
consumer fireworks, sparking composition, spark
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Principles
of Solid Rocket Motor Design |
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Naminosuke Kubota
Scientific Advisor, Mitsubishi Electric Corporation, Kamimachiya 325,
Kamakura 247-0065, Japan |
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Abstract: A number of parameters
are needed to design a rocket motor to satisfy the specified flight
trajectory of its payload. The major components of a rocket motor
are propellant grain, motor case and its insulation, nozzle, and
igniter. One of the key parameters is the burn rate characteristic
of the propellant grain that is set in a rocket chamber either by
cast method or by free-stand. The combustion phenomena in the motor
are highly dependent on the design of the perforated propellant
grains in which transient burning, erosive burning, oscillatory
burning, and unstable burning occur. As a special rocket motor design,
a two stage motor with two propellant grains in a single chamber,
is described and compared with practical firing test results.
Keywords: flight dynamics,
rocket motor, propellant combustion, two-stage motor, igniter, propellant
grain, nozzle
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A
Practical Performance Testing Protocol for Fireworks Mortar Tubes
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Andrew Fischer +
Pyromite Pyrotechnic Services, Melbourne, Victoria, Australia |
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Abstract: The author’s development
of an alternative design for a fireworks mortar coincided with the
restructure of regulations concerning display fireworks in the State
of Queensland, Australia. This new Code of Practice for the Display
of Outdoor Fireworks has a requirement for manufacturers of equipment
to develop performance-based tests that will prove the safety and
suitability of plant and equipment used. The authorities proposed
that a mortar tube was to be given a service life of five years.
This article describes a protocol that has been successfully put
into practice to test the new mortar tube. The protocol is called
the Five Year Accelerated Test Program or “FYATP”.
Keywords: mortar, plastic tube,
service life, polyethylene mortar
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Fireworks
Shells Subjected To a Modified Height-To-Detonation Test |
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E. Contestabile, R. Guilbeault, D. Wilson,
and B. von Rosen Canadian Explosives
Research Laboratory (CERL), Natural Resources Canada, Ottawa, Canada |
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Abstract: Initiation of fireworks
articles, as by a fire, can result in communication to adjacent articles
and at times transition to a mass explosion. Such an event can be
catastrophic. In a quest to discover the process by which this transition
occurs and thereby work to mitigate it so as to prevent the dire consequences,
a series of research programs was established. This paper reports
the findings of attempts to cause communication within a linear array
of fireworks shells confined in steel pipes and to measure the shell-to-shell
communication rate. The array of shells was initiated with an explosive
booster charge.
The findings indicate that such an array, with the given confinement
and initiation stimulus, is not conducive to the sympathetic initiation
of the tested fireworks shells.
Keywords: height-to-detonation,
HtD, fireworks aerial shell, VoD probe, rate of propagation, RoP,
explosion test
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Communications
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A Simplified Method for Determining
the Strength of a Tube Subjected to Internal Pressure by L. Weinman
Reprint
Information: Number of pages = 2.
Review by John Steinberg of: Amateur
Rocket Motor Construction David Sleeter
Review by K. Koenig of: Rocket Propulsion Elements, Seventh
Edition by George P. Sutton, Oscar Biblarz
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