Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Download A Study Of The Gas Phase Chemistry Of Solid Propellants Using A Microprobe Mass Spectrometer Mpms System Preliminary Results For Solid Fuels Htpb Zecorez And Bamo Nmmo Single Base Propellant M10 And An Rdx Based Propellant Blx 9 full books in PDF, epub, and Kindle. Read online A Study Of The Gas Phase Chemistry Of Solid Propellants Using A Microprobe Mass Spectrometer Mpms System Preliminary Results For Solid Fuels Htpb Zecorez And Bamo Nmmo Single Base Propellant M10 And An Rdx Based Propellant Blx 9 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author :
Publisher :
ISBN 13 :
Total Pages : 308 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Study of the Gas Phase Chemistry of Solid Propellants Using a Microprobe Mass Spectrometer (MPMS) System: Preliminary Results for Solid Fuels (HTPB/Zecorez and BAMO/NMMO) Single-Base Propellant (M10) and an RDX-Based Propellant (BLX-9). written by and published by . This book was released on 1991 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed knowledge of the gas-phase reactions which occur during propellant ignition and combustion are required to understand and model these processes. If detailed models were available, modification of propellant formulations for improved combustion behavior could be achieved with much less trial-and-error testing. Furthermore, detailed models could be used to generate simplified kinetics schemes for use in propellant models. The present research program, centers around the development and application of a microprobe, mass spectrometer (MPMS) system to study the gas phase chemistry of solid propellant ingredients and solid propellants during heating by a CO2 laser and during steady combustion. The MPMS system uses quartz microprobes with orifice sizes of 100 microns or less to withdraw gases from the region above the sample material. Through a two stage pumping system, the sample is delivered to a quadrupole mass spectrometer for analysis. Sampling is continuous throughout the combustion event so that species profiles of stable intermediates above the sample are obtained during the experiments. In addition to the MPMS system, existing experimental methods to be used in the work include high speed direct photography, high speed schlieren photography, microthermocouple probes and photodiodes (for first visible light).
Author :
Publisher :
ISBN 13 :
Total Pages : 764 pages
Book Rating : 4.:/5 (3 download)
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1991-09 with total page 764 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1322 pages
Book Rating : 4.3/5 (129 download)
Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 1322 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Study of Gas Phase Chemistry of Solid Propellants Using a Microprobe Mass Spectrometer System. Results for RDX, BLX-9, XM-39, M9 and JA-2 written by and published by . This book was released on 1991 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research program is designed to address the critical need for data on the gas-phase chemistry of solid propellants through the development and application of a microprobe mass spectrometer (MPMS) system. The MPMS system is being used to study the gas-phase chemistry occurring above solid propellant ingredients and actual solid propellants when they are heated and/or ignited by the heat flux from a CO2 laser. In addition to the MPMS system, direct and Schlieren photography are being used to study the flame structure and twenty- five micron thermocouples are being used to measure the gas-phase temperature profile. During the last year nearly fifty tests were performed with neat RDX as well as with composite, XM-39 and BLX-9, and double-base propellants, M-9 and JA-2. Measurements of gas-phase species and temperature profiles for neat RDX and tow RDX composite propellants show that while the chemical species detected are similar, the gas-phase structure for these propellants is significantly different. For incident laser energy fluxes above 100 W/sq cm, all three propellants exhibited a primary flame caused by the reaction of CH2O and NO2. The mole fraction of CH2O at or near the sample surface was approximately 0.20 for RDX and XM39 but was about 0.33 for BLX9 due to the addition of CH2O from the decomposition of the BTTN energetic plasticizer. The primary flame products consisted of significant amounts of NO for all three propellants and CO for the composites along with smaller amounts of H2O for RDX and BLX9, CO2 for RDX and XM39, and h2 for RDX.
Author :
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Study of the Gas Phase Chemistry of Solid Propellants Using a Microprobe Mass Spectrometer (MPMS) System: Initial Development of the MPMS System written by and published by . This book was released on 1990 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed knowledge of the gas-phase reactions which occur during propellant ignition and combustion are required to understand and model these processes. If detailed models were available, modification of propellant formulations for improved combustion behavior could be achieved with much less trail-and-error testing. Furthermore, detailed models could be used to generate simplified kinetics schemes for use in propellant models. Without a firm basis for these simplified kinetic schemes, the kinetic parameters are often adjusted to fit burning rate and ignition data; thus the propellant models are reduced to sophisticated curve fits to experimental data. The present research program, centers around the development and application of a microprobe, mass spectrometer (MPMS) system to study the gas phase chemistry of solid propellant ingredients and solid propellants during heating by a CO2 laser and during steady combustion. The MPMS system uses quartz microprobes with orifice sizes of 100 microns or less to withdraw gases from the region above the sample material. Through a two stage pumping system, the sample is delivered to a quadrupole mass spectrometer for analysis. Sampling is continuous throughout the combustion event so that species profiles of stable intermediates above the sample are obtained during the experiments.
Author :
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Study of the Gas-Phase Chemistry of Solid Propellant Ingredients Using CO2 Laser Heating written by and published by . This book was released on 1991 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research program is designed to address the critical need for data on the gas phase chemistry of solid propellants through the development and application of a Microprobe Mass Spectrometer (MPMS) system. The MPMS systems is being used to study the gas-phase chemistry occurring above solid propellant ingredients and actual solid propellants when they are heated and/or ignited by the heat flux from a Carbon dioxide laser. Currently the MPMS system uses quartz microprobes with orifice sizes of twenty microns which results in a spatial resolution of approximately 100 microns. In addition to the MPMS system, direct and Schlieren photography are being used to study the flame structure and twenty-five micron thermocouples are being used to measure the gas-phase temperature profile. The specific goal of this research is to obtain detailed species profiles of the major reacting species above the surface of the individual propellant ingredients and actual propellants in order to obtain an improved understanding of the controlling chemical processes and of the interactions of binders and oxidizers in heterogeneous propellants. In the testing both heterogeneous and homogeneous propellants are being studied as well as their individual ingredients.
Author :
Publisher :
ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Study of Solid Propellants Using a Microprobe Mass Spectrometer System written by and published by . This book was released on 1993 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this work is to determine the chemical mechanisms of solid propellant ignition and deflagration with an emphasis on the decomposition of individual propellant ingredients and on the gas phase reactions of the products of decomposition. A quadrupole mass spectrometer system using quartz microprobes measures species profiles above the surface of the sample during CO2 laser induced pyrolysis or during laser assisted deflagration of the sample. In addition microthermocouples are used to measure the surface temperature and gas phase temperatures during testing. To complement the experimental studies, chemical kinetic models produced by other researchers are used to model some of the data obtained. jg p.4.
Author : T.L. Varghese
Publisher : Allied Publishers
ISBN 13 : 9385926330
Total Pages : 326 pages
Book Rating : 4.3/5 (859 download)
Download or read book The Chemistry and Technology of Solid Rocket Propellants (A Treatise on Solid Propellants) written by T.L. Varghese and published by Allied Publishers. This book was released on 2017-03-29 with total page 326 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book is a treatise on solid propellants in nine chapters, covering the history, chemistry, energetics, processing and characterization aspects of composite solid propellants, internal ballistics, advanced solid propellants, safety, quality and reliability and homogenous or double base propellants. The book also traces the evolution of solid propellant technology in ISRO for launch vehicles and sounding rockets. There is a detailed table of contents, expanded index, glossary, exhaustive references and questions in each chapter. It can be used as a textbook for science and engineering students, as a reference book for researchers and as a companion to scientists and engineers working in the research, development and production areas of solid propellants.
Author : Vigor Yang
Publisher : AIAA
ISBN 13 : 9781600864377
Total Pages : 1038 pages
Book Rating : 4.8/5 (643 download)
Download or read book Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 written by Vigor Yang and published by AIAA. This book was released on 2000 with total page 1038 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Yu Chen
Publisher :
ISBN 13 : 9781536180541
Total Pages : 298 pages
Book Rating : 4.1/5 (85 download)
Download or read book An Introduction to Propellants written by Yu Chen and published by . This book was released on 2020-07-22 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: Solid propellant is the most important energy source for rocket, missile and other weapons to launch, and is the key material to realize the firing range and damage effect of weapons. In order to meet the requirements of weapon application, the overall requirements for the energy performance, combustion performance, mechanical performance, storage performance, safety performance and process performance of solid propellant are put forward. Therefore, there are many challenges to fully meet the requirements of solid propellant and apply it to weapons. In recent years, with the development of material science, computational science and experimental technology, there are many reports about the composition, structure, performance research and prediction of solid propellants.This book reviews the research progress in solid propellant binder, energy performance prediction and thermodynamic calculation, combustion gas flow and combustion performance regulation, material storage performance research and safety performance simulation, and discusses the key development direction. The summary and prospect of this paper are expected to provide guidance, reference and inspiration for relevant researchers to carry out the research of solid propellant.This book is suitable for researchers, technicians and students who are engaged in solid propellant, weapons, chemistry and other work to read, for reference in specific research work. Due to the limited level of editors and short time, some problems are inevitable. We regret for some problems.
Author : Naminosuke Kubota
Publisher : Wiley-VCH
ISBN 13 :
Total Pages : 544 pages
Book Rating : 4.3/5 (91 download)
Download or read book Propellants and Explosives written by Naminosuke Kubota and published by Wiley-VCH. This book was released on 2007 with total page 544 pages. Available in PDF, EPUB and Kindle. Book excerpt: Demonstrated by the use of a number of colored photographs during burning. New applications of energetic materials such as pyrolants and ducted rockets for an advanced propulsion system are also described.
Author : Alpheus Messerly Ball
Publisher :
ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (319 download)
Download or read book Solid Propellants written by Alpheus Messerly Ball and published by . This book was released on 1964 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Martin Summerfield
Publisher : AIAA
ISBN 13 : 9781600863967
Total Pages : 922 pages
Book Rating : 4.8/5 (639 download)
Download or read book Nonsteady Burning and Combustion Stability of Solid Propellants written by Martin Summerfield and published by AIAA. This book was released on 1992 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 57 pages
Book Rating : 4.:/5 (227 download)
Download or read book Condensed-Phase Processes During Solid Propellant Combustion. Part 2: Chemical and Microscopic Examination of Conductively Quenched Samples of RDX, XM39, JA2, M30, and HMX-Binder Compositions written by and published by . This book was released on 1992 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt: Burning propellant samples were quenched, and the burned surfaces were examined microscopically and by chemical analysis. Studies are in progress on a series of propellants including XM39, M30, JA2, RDX, and HMX-polyester compositions. The results to date are consistent with the idea that at least at low pressures (below 2.0 MPa), a liquid layer forms during combustion of most of the propellants, with the possible exception of JA2; scanning electron microscope examination shows the existence of a liquid layer but does not provide evidence of degradation below this layer. The effect of composition and pressure on this liquid layer is discussed. Further gas chromatography mass spectrometry analysis confirms our earlier result that at least in the case of XM39, the stabilizer is depleted considerably in the surface layers, presumably by reaction with nitrogen oxides formed by decomposition of RDX and NC. Further high performance liquid chromatography results confirm our earlier result that for XM39, HMX2, and RDX (which contain the cyclic nitramines HMX and RDX), there is a significant increase in concentration of the mechanistically significant nitrosamines MRDX and DRDX over the very small amounts possibly present as impurities In RDX and HMX. FTIR-PAS results provide evidence for condensed-phase reaction in M30 and JA2.
Author : North Atlantic Treaty Organization. Combustion and Propulsion Panel
Publisher : Pergamon
ISBN 13 :
Total Pages : 680 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Chemistry of Propellants written by North Atlantic Treaty Organization. Combustion and Propulsion Panel and published by Pergamon. This book was released on 1960 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael A. Schroder
Publisher :
ISBN 13 :
Total Pages : 31 pages
Book Rating : 4.:/5 (227 download)
Download or read book Condensed-Phase Processes During Solid Propellant Combustion. 1. Preliminary Chemical and Microscopic Examination of Extinguished Propellant Samples written by Michael A. Schroder and published by . This book was released on 1990 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: Burning propellant samples are quenched, and the burned surfaces are examined microscopically and by chemical analysis. Studies are in progress on a series of propellants including XM39, M30, JA2, RDX, HMX, HMX/PU, and HMP/polyester ('HMX2') compositions. Preliminary results on quenched samples of XM39 burned at low pressures show evidence of a liquid layer approximately 100-300 micron thick. SEM examination reveals little if any evidence of degradation below this liquid layer. GCMS analysis shows that the stabilizer is depleted considerably in the surface layers of quenched samples, presumably by reaction with nitrogen oxides formed by decomposition of RDX and NC. HPLC results show that there is a significant increase the very small amounts possibly present as impurities. Keywords: Extinguishment, Quenched-sample analysis, Propellants, Explosives, Nitramines, Nitrate esters, Combustion. (jes).
