Heterogeneous Reactions on Aluminum Oxide Surfaces Modeling Rocket Exhaust Particles

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Book Synopsis Heterogeneous Reactions on Aluminum Oxide Surfaces Modeling Rocket Exhaust Particles by :

Download or read book Heterogeneous Reactions on Aluminum Oxide Surfaces Modeling Rocket Exhaust Particles written by and published by . This book was released on 1999 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research was performed by a graduate student, and post-doctoral research fellow. Our studies for the hydroxylation and dehydroxylation of a-Al2O3 (001) led to two publications. The adsorption of H2O on a-Al2O3 (001) was accepted and published in the Journal of Physical Chemistry. The desorption of H2O from a-Al2O3 (001) was accepted and published in Surface Science. The study of HCl adsorption and desorption from a-Al1O3 (001) led to one publication in Surface Science. In addition, the study of HCl and H2O adsorption on a Al2O3 (001) and the displacement of Al-OH surface species by HCl and displacement of Al-Cl surface species by H2O led to one additional manuscript that is still under review. Since the conclusion of this research grant, we have continued to examine the surface chemistry of amorphous Al2O3 surfaces. Oxide surface chemistry is still a largely unexplored area. Our surface reactivity studies have helped to define this new territory in surface science. These studies have also improved our understanding of heterogeneous reactions on aluminum oxide rocket exhaust particles in the atmosphere.

Heterogeneous Chemistry on Metal Oxide Surfaces of Interest for the Stratospheric Effects of Solid Rocket Motor Exhaust

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Total Pages : 12 pages
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Book Synopsis Heterogeneous Chemistry on Metal Oxide Surfaces of Interest for the Stratospheric Effects of Solid Rocket Motor Exhaust by :

Download or read book Heterogeneous Chemistry on Metal Oxide Surfaces of Interest for the Stratospheric Effects of Solid Rocket Motor Exhaust written by and published by . This book was released on 1995 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: The emissions from solid rocket motors (SRMs) include hydrogen chloride vapor (HCl) and other inorganic chlorine compounds, as well as aluminum oxide particles. The effects of these emissions on stratospheric ozone have been investigated by Prather et al. 1, Pyle2, and others. Even though such effects are not evident from satellite observations following a Space Shuttle launch 3, it is possible for the perturbation to be quite pronounced in the immediate neighborhood of the rocket plume.

Single Particle Studies of Heterogeneous Atmospheric Chemistry on Aluminum Oxide Particles in a Quadrupole Trap

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Book Synopsis Single Particle Studies of Heterogeneous Atmospheric Chemistry on Aluminum Oxide Particles in a Quadrupole Trap by :

Download or read book Single Particle Studies of Heterogeneous Atmospheric Chemistry on Aluminum Oxide Particles in a Quadrupole Trap written by and published by . This book was released on 2000 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents a research program consisting of laboratory and field measurements investigating the atmospheric chemistry and aerosol microphysics of the impacts of rocket motor exhausts on upper atmospheric chemical cycles and ozone. The experimental investigation employs a laboratory quadrupole trap electrodynamic levitation apparatus to study heterogeneous processes on single aluminum oxide particles representative of those exhausted into the atmosphere by solid rocket motors. We have investigated the activities of different types of aluminum oxide particles for uptake of gas-phase H2O and HCl. The particle types investigated were alpha-Al2O3, gamma-Al2O3, H2SO4-treated alpha-Al2O3, H2SO4-treated gamma-Al2O3, and metastable aluminum oxide formed by rapid cooling from molten Al2O3 in a shock tube, analogous to particle processing in a rocket exhaust nozzle. Particles were treated with H2SO4 by vapor deposition in an oven. The kinetic measurements consisted of independent, simultaneous observations of mass uptake and particle size increase upon exposure of single particles to fixed concentrations of H2O or HCl in slowly flowing gas mixtures at 1 atm and temperatures from 300 K to 190 K. alpha-Al2O3 and gamma-Al2O3 were essentially inert toward H2O and HCl uptake, however they readily adsorbed monolayer-equivalent levels of H2SO4 vapor, and H2SO4-coated and metastable particles were active toward H2O and HCI uptake. The measured uptake efficiencies imply fast reaction rates within rocket exhaust plumes, potentially leading to CCN behavior as well as heterogeneous chlorine activation by these particles. The field measurements consisted of in situ ozone mixing ratio measurements on the NASA WB57-F high altitude aircraft, as part of a suite of instrumentation designed to characterize the chemistry and dynamics of rocket exhaust plumes in the lower stratosphere.

Adsorption and Chemical Reaction of Gaseous Mixtures of Hydrogen Chloride and Water on Aluminum Oxide and Application to Solid-propellant Rocket Exhaust Clouds

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Total Pages : 42 pages
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Book Synopsis Adsorption and Chemical Reaction of Gaseous Mixtures of Hydrogen Chloride and Water on Aluminum Oxide and Application to Solid-propellant Rocket Exhaust Clouds by : Wesley R. Cofer

Download or read book Adsorption and Chemical Reaction of Gaseous Mixtures of Hydrogen Chloride and Water on Aluminum Oxide and Application to Solid-propellant Rocket Exhaust Clouds written by Wesley R. Cofer and published by . This book was released on 1978 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Heat Transfer Model for Aluminum Oxide Particles Within a Solid Fuel Rocket Exhaust Plume

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ISBN 13 :
Total Pages : 218 pages
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Book Synopsis A Heat Transfer Model for Aluminum Oxide Particles Within a Solid Fuel Rocket Exhaust Plume by : David Wilson Young

Download or read book A Heat Transfer Model for Aluminum Oxide Particles Within a Solid Fuel Rocket Exhaust Plume written by David Wilson Young and published by . This book was released on 1986 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Characteristics of Alumina Particles from Solid Rocket Motor Exhaust in the Stratosphere

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Total Pages : 42 pages
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Book Synopsis Characteristics of Alumina Particles from Solid Rocket Motor Exhaust in the Stratosphere by :

Download or read book Characteristics of Alumina Particles from Solid Rocket Motor Exhaust in the Stratosphere written by and published by . This book was released on 1995 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on currently available data, a unified model for the particle size distribution, particle density, and geometrical dispersion for the alumina particles in the exhaust of a Titan SRM plume in the stratosphere is presented. The particle size distribution is found to be trimodal with Sauter mean diameters of 0.056, 1.0, and 3.6 um for the small, medium, and large size modes, respectively. Nearly all the particles lie within the small size mode, but nearly all the mass lies in the large size mode. About two-thirds of the particle surface area available for heterogeneous chemical reactions is due to the large particle mode while most of the remaining surface area is due to the small particle mode. The light scattering characteristics of the plume were also explored. Mie scattering calculations were used to predict the local attenuation of the plume as a function of wavelength and the total attenuation of a beam of radiation through the plume making an arbitrary angle with respect to the axis of the plume and as a function of time after SRM passage for several wavelengths in ultraviolet, visible, and infrared spectral regions. These studies show that most of the attenuation is due to the large-size mode. An expression for the volume density of total area of the particles is derived in terms of known parameters and the Sauter mean diameter. Mie theory is then used to show that this Sauter mean diameter can be measured using a two-color transmissometer.

Heterogeneous Chemistry in Solid Rocket Motor Plumes

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Total Pages : 18 pages
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Book Synopsis Heterogeneous Chemistry in Solid Rocket Motor Plumes by :

Download or read book Heterogeneous Chemistry in Solid Rocket Motor Plumes written by and published by . This book was released on 1997 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reaction rates of ozone decomposition and adsorption/desorption rates of HCl on aluminum oxide (alumina) particles were measured by a new technique involving real-time ultraviolet absorption spectroscopy in a static reactor. Reaction probabilities eta are reported for ozone on alpha-alumina, gamma-alumina, and chromatographic alumina (hydoxylated alumina), respectively, over the temperature range -60 to 200 deg C. These measurements expand on previous measurements from this group using a flow tube reactor. The adsortion/desorption kinetics is a new effort that addresses the key issue of whether heterogeneous chemistry, such as the reaction HCl + ClONO2 --> Cl2 + HNO3, on alumina particles is a significant reaction mechanism for global stratospheric ozone depletion.

Review of Aluminium Oxide Rocket Exhaust Particles

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Book Synopsis Review of Aluminium Oxide Rocket Exhaust Particles by : R. A. Reed

Download or read book Review of Aluminium Oxide Rocket Exhaust Particles written by R. A. Reed and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Heterogeneous Reactions of Micro and Nano Aluminum Particles with Various Oxidizers

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Book Synopsis Heterogeneous Reactions of Micro and Nano Aluminum Particles with Various Oxidizers by : Florin Saceleanu

Download or read book Heterogeneous Reactions of Micro and Nano Aluminum Particles with Various Oxidizers written by Florin Saceleanu and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Micro and nano aluminum (Al) particles have drawn much attention for properties as metal fuels in energetic materials. Aluminum is the preferred metal due to its thermodynamic stability after long term storage, abundance on Earth and relatively high reactivity with various oxidizers such as oxygen gas, metal oxides and liquid water. This thesis investigates the kinetics of heterogeneous reactions of micro and nano aluminum particles via controlled oxidation and combustion experiments. The main objectives of this research are to incorporate fundamental theories in solid state kinetics with the experimental data/observations, and obtain a deeper understanding of the kinetic mechanisms that control these heterogeneous reactions. Proper experimental setups and procedures are an essential part of this research due to the currently limited theoretical knowledge in this field. Studies have shown that mass diffusion and phase transformations processes are elementary for reactions of Al in air or oxygen. However, the physical processes regarding simultaneous oxidation and phase transformation were unclear. Thermogravimetric and differential scanning calorimetry experiments and the core-shell model of oxidation were combined, and it was found that this model is only applicable when the shell does not undergo phase transformations. On the other hand, the simultaneous oxidation and phase transformation were explained by the nucleation and growth model with a parameter that defines the rate controlling processes. Diffusional processes were rate determining steps in the oxidation of micro and nano Al powders while the kinetics of the chemical reactions were very fast. Similarly, high speed imaging of the combustion of consolidated Al particles via laser ignition in a closed chamber at various partial pressures of oxygen indicated that oxygen diffusion is the rate controlling mechanism of flame propagation. However, some experimental observations diverge from the theoretical predictions due to the particle agglomeration and inhomogeneous pore structure. Aluminum based thermites are a class of highly energetic materials composed of solid state Al and metal oxidizer with tunable combustion properties. The ignition and combustion mechanisms of consolidated aluminum/copper oxide (CuO) nanothermite pellets were investigated via laser ignition coupled with high speed imaging. It was found that the fast heating created significant material ablation followed by heat transfer along the heated surface. The bulk ignition occurred near the edges prior to the self-sustained combustion. The high porosity Al/CuO pellets ignited significantly faster and the burning speed was orders of magnitude higher compared to the low porosity pellets. The results indicated that the reaction mechanism changed from mass convection to heat conduction with increasing the bulk density. Scanning electron microscopy images of pre and post-combustion illustrated that homogeneity of the mixture is a critical parameter for optimizing the performance. On the other hand, the type of nanothermite structures is a critical parameter for the tenability of these reactions. It was found that the ignition mechanisms of the consolidated Al/CuO nanoparticles and sputtered Al/Cu2O nanolaminates are fundamentally different. The net energy balance on the laser heated surface controlled the ignition delay in the pellets, and this was dominated by the net thermal conductivity of the porous structure. A semi-empirical laser ignition model of the pellets was proposed. On the other hand, significant laser energy absorption was mandatory for the ignition of nanolaminates. The ignition delay was optimized by finding the optimum Cu2O layer thickness that maximized both the absorption coefficient of laser radiation and the mass diffusion rates of oxygen. The reactions between aluminum and liquid water are attractive to generated hydrogen gas on-demand. Controlled oxidation experiments were performed using isothermal calorimetry and self-sustained combustion experiments were performed using a high pressure batch reactor. . It was found that the nucleation and growth of the aluminum hydroxides byproducts control the kinetics of these reactions and thus the kinetics of hydrogen release. Model and model-free methods were implemented to describe the reaction sequence. It was found that this mechanism exhibits two distinct and sequential stages: a kinetically controlled stage where nucleation and growth is limited by the chemical reactions on the surface of aluminum, and a diffusion controlled stage where the growth is limited by the mass diffusion through the aluminum hydroxide by-products. The separation of these stages is not obvious under non-isothermal conditions due to the overlap of the stages, and the one with a lower Ea dominates. The kinetics of the reactions was significantly increased under high temperature and pressure, which prevented the boiling of water. The Al-hydroxide byproducts and NaOH solutions were found to have catalytic properties on the Al/water reactions by lowering the apparent activation energy. A semi-empirical batch reactor model was proposed to study the complexity of these heterogeneous reactions.

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

92-3365 - 92-3399

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ISBN 13 :
Total Pages : 414 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 92-3365 - 92-3399 by :

Download or read book 92-3365 - 92-3399 written by and published by . This book was released on 1992 with total page 414 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Feasibility Study for Methods of Determining Crystal Phase of Aluminum Oxide (AL2O3) Rocket Exhaust Particles

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Total Pages : 50 pages
Book Rating : 4.:/5 (181 download)

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Book Synopsis Feasibility Study for Methods of Determining Crystal Phase of Aluminum Oxide (AL2O3) Rocket Exhaust Particles by : Keith M. Dill

Download or read book Feasibility Study for Methods of Determining Crystal Phase of Aluminum Oxide (AL2O3) Rocket Exhaust Particles written by Keith M. Dill and published by . This book was released on 1988 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Laboratory Studies of the Stratospheric Effects of Rocket Exhaust

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Total Pages : 29 pages
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Book Synopsis Laboratory Studies of the Stratospheric Effects of Rocket Exhaust by : M. Molina

Download or read book Laboratory Studies of the Stratospheric Effects of Rocket Exhaust written by M. Molina and published by . This book was released on 1998 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt: The most important chlorine activation reaction that takes place in the stratosphere is the heterogeneous reaction of chlorine nitrate with hydrogen chloride to produce molecular chlorine and nitric acid. The reaction is catalytic, promoted by surfaces that are not themselves affected by the reaction. This process was investigated in the laboratory: the reaction probability was found to have a value of about 0.02 on glass, on laboratory alumina, and on alumina particles emitted by solid rocket motors. The reaction probability on ice surfaces has a value larger than 0.2 and a negligible value on halocarbon wax or Teflon surfaces. The measurements were carried out under reactant partial pressure, temperature and humidity conditions covering those that are encountered in the mid-latitude lower stratosphere. The reaction mechanism appears do be determined by the water layers adsorbed on the solid surface. Measurements of the amount of water taken up by alumina surfaces were also carried out; the results indicate that under stratospheric conditions several water layers will indeed cover the alumina surfaces.

Solidification Kinetics of Alpha Versus Gamma Formation of Aluminum Oxide (Al2O3) Particles in Solid Propellant Rocket Exhausts

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Total Pages : 112 pages
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Book Synopsis Solidification Kinetics of Alpha Versus Gamma Formation of Aluminum Oxide (Al2O3) Particles in Solid Propellant Rocket Exhausts by : Suzanne Moore Oliver

Download or read book Solidification Kinetics of Alpha Versus Gamma Formation of Aluminum Oxide (Al2O3) Particles in Solid Propellant Rocket Exhausts written by Suzanne Moore Oliver and published by . This book was released on 1991 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Solid Rocket Motor Performance Analysis and Prediction

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ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Solid Rocket Motor Performance Analysis and Prediction by : William H. Miller

Download or read book Solid Rocket Motor Performance Analysis and Prediction written by William H. Miller and published by . This book was released on 1971 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Model of Chlorocarbon (CFC-12) Chemisorption on Solid Rocket Motor Alumina Exhaust Particles

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ISBN 13 :
Total Pages : 216 pages
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Book Synopsis Model of Chlorocarbon (CFC-12) Chemisorption on Solid Rocket Motor Alumina Exhaust Particles by : Gary E. Lund

Download or read book Model of Chlorocarbon (CFC-12) Chemisorption on Solid Rocket Motor Alumina Exhaust Particles written by Gary E. Lund and published by . This book was released on 1995 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Particle Size Measurement of Aluminium Oxide in a Solid Propellant Rocket Exhaust

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Book Synopsis Particle Size Measurement of Aluminium Oxide in a Solid Propellant Rocket Exhaust by : Alan Rose

Download or read book Particle Size Measurement of Aluminium Oxide in a Solid Propellant Rocket Exhaust written by Alan Rose and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: