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Methodology for Designing Gas Generator
Systems for the Instantaneous
Personal Protection System, 18-9136
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Principal Investigators
P. A. Cox
Walter M. Gray
Inclusion Dates: 03/01/99 - Current
Background - The major goal of this program is
to develop at SwRI the technology to design inflation systems. Special emphasis will be
placed on application to the SwRI-developed instantaneous personal protection system
(IPPS), but the technology will be applicable to inflation systems in general.
Approach - Development of the design
methodologies will require engineering models to describe bag inflation and the
solid-propellant gas-generating processes. The approach calls for the use of available
analytical and numerical models, similitude analysis, and carefully designed experiments
to generate an easy-to-use engineering model. Independent models will first be developed
for bag inflation and gas generation. The models will then be merged to describe the
complete system. The teams intent is to develop either a personal computer-based or
a nondimensional graphical model that captures the essential physics of the gas-generation
and inflation processes without the mathematical complexities. Graphical similitude models
are typically developed from extensive experimental data. In this program, much of the
data will be generated through the application of analytical and numerical models that
have been validated by experiment. Finally, all the analytical, numerical, and
experimental results will be statistically analyzed to develop a similitude model.
Accomplishments - Models have been developed
to describe propellant combustion, venting from the combustion chamber, venting from a
high-pressure reservoir of compressed gas, and erection of the IPPS system. The models
have been combined to provide a numerical simulation of the process from propellant
initiation through erection of the IPPS system. Preliminary calculations have indicated
the high gas temperature may create problems in a system driven totally by burning
propellant. Simulations to date have been with gun propellants for which data already
exist. Gun propellants have high burning rates that are probably too high for the IPPS
system. Characterizations are being sought for a variety of different propellants with a
wide range of pressure-dependent burning rates to determine which propellants can best
meet IPPS system requirements.
Materials Research and
Structural Mechanics Program
1999 IR&D Home SwRI Home
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