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Studies Of The Exhaust Products From Solid Propellant Rocket Motors
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Book Synopsis Studies of the Exhaust Products from Solid Propellant Rocket Motors by : R. Dawbarn
Download or read book Studies of the Exhaust Products from Solid Propellant Rocket Motors written by R. Dawbarn and published by . This book was released on 1976 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Rocket Propulsion Technology by : A. Davenas
Download or read book Solid Rocket Propulsion Technology written by A. Davenas and published by Newnes. This book was released on 2012-12-02 with total page 623 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.
Book Synopsis Experimental Study of Liquid Rocket Simulation of Solid Propellant Rocket Exhaust Characteristics by : L. JABLANSKY
Download or read book Experimental Study of Liquid Rocket Simulation of Solid Propellant Rocket Exhaust Characteristics written by L. JABLANSKY and published by . This book was released on 1964 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A substantial cost saving can be realized if a small liquid propellant rocket engine, using cheap propellants, can be used to screen nozzle materials for eventual use with large solid rocket motors using costly propellants. Work was completed in which the nozzle erosion experienced in a solid rocket motor using AHH propellant was simulated by a liquid propellant engine using white fuming nitric acid and benzene. The work was conducted at a one-to-one scale ratio and the approach taken was to simulate erosion by simulating nozzle environment. Approximate simulation of nozzle erosion was achieved. Additional work is recommended to perform simulation of aluminized propellants and study scaling effects. (Author).
Book Synopsis A Study of Solid-propellant Rocket Motor Exposed Materials Behavior by :
Download or read book A Study of Solid-propellant Rocket Motor Exposed Materials Behavior written by and published by . This book was released on 1964* with total page 83 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives of the study: (a) To develop design tools, in the form of digital computer programs, for the nozzle designer to use for calculating the behavior of materials exposed to a solid-propellant rocket-exhaust environment. (b) To marshall existing theoretical methods, or develop new methods, to gain a better understanding of the fundamental mechanisms. Work was directed toward development of two digital-computer programs. One is applicable to materials such as graphite and tungsten, that, erode with one moving boundary or do not erode at all. The other applicable to the reinforced plastic materials that form a char layer. Effort in the areas of transient conduction, equilibrium chemistry, reaction kinetics, and mass transport, as applied to the solid-propellant rocket problem, is described in detail. (See also AD-428 437).
Book Synopsis Design and Evaluation of a Turbojet-exhaust Simulator with a Solid-propellant Rocket Motor for Free-flight Research by : Abraham Leiss
Download or read book Design and Evaluation of a Turbojet-exhaust Simulator with a Solid-propellant Rocket Motor for Free-flight Research written by Abraham Leiss and published by . This book was released on 1957 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of Solid-propellant Rocket Motor Exposed Materials Behavior by :
Download or read book A Study of Solid-propellant Rocket Motor Exposed Materials Behavior written by and published by . This book was released on 1964 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives of the study: (a) To develop design tools, in the form of digital computer programs, for the nozzle designer to use for calculating the behavior of materials exposed to a solid-propellant rocket-exhaust environment. (b) To marshall existing theoretical methods, or develop new methods, to gain a better understanding of the fundamental mechanisms. Work was directed toward development of two digital-computer programs. One is applicable to materials such as graphite and tungsten, that, erode with one moving boundary or do not erode at all. The other applicable to the reinforced plastic materials that form a char layer. Effort in the areas of transient conduction, equilibrium chemistry, reaction kinetics, and mass transport, as applied to the solid-propellant rocket problem, is described in detail. (See also AD-428 437).
Book Synopsis Fundamentals of Rocket Propulsion by : DP Mishra
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Book Synopsis An Experimental Investigation of the Effect of High-pressure Tailpipe Length on the Performance of Solid-propellant Motors for Rocket-powered Aircraft by : Charles J. Rodriguez
Download or read book An Experimental Investigation of the Effect of High-pressure Tailpipe Length on the Performance of Solid-propellant Motors for Rocket-powered Aircraft written by Charles J. Rodriguez and published by . This book was released on 1952 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Solid Propellant Grain Structural Integrity Analysis by : James S. Noel
Download or read book Solid Propellant Grain Structural Integrity Analysis written by James S. Noel and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Liquid Rocket and Propellants by : L.E. Bollinger
Download or read book Liquid Rocket and Propellants written by L.E. Bollinger and published by Elsevier. This book was released on 2013-04-22 with total page 699 pages. Available in PDF, EPUB and Kindle. Book excerpt: Liquid Rocket and Propellants
Book Synopsis Research on Ablative Plastic Characterization in Simulated Motor Exhaust by : S. L. Ostrow
Download or read book Research on Ablative Plastic Characterization in Simulated Motor Exhaust written by S. L. Ostrow and published by . This book was released on 1967 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt: New chemical compositions and physical constructions of ablative materials were exposed in three rocket motor combustion-gas environments to determine the potential usefulness of these materials for hyperenvironmental conditions associated with current and future solid and liquid propellant motors. These gas environments were: (1) the exhaust from a high-temperature Aeronutronic solid propellant rocket motor simulator, a nitrogen tetroxide (N2O4)-50 percent hydrazine and 50 percent unsymmetrical dimethylyhydrazine (50-50) liquid propellant environment, and a chlorine trifluoride (CTF)-hydrazine (N2H4) liquid propellant environment. Material erosion and thermal insulation characteristics of the research nozzles were evaluated by comparisons of chamber pressure versus time data, erosion and resin degradation rates, and visual photographic data. Eight nozzle specimens, comprising test series 1, were exposed to the exhaust environment of a storable liquid propellant rocket motor utilizing N2O4/50-50 at a chamber pressure of 700 psia. Twenty-five nozzle specimens (comprising test series 2) were exposed to the exhaust environment of a simulated solid propellant at a chamber pressure of 500 psia; flame temperature was 5800 F and the propellant was highly aluminized. Eight nozzle specimens, comprising test series 3, were exposed to the exhaust environment of another storable liquid propellant rocket motor utilizing CTF/N2H4 at a chamber pressure of 500 psia.
Book Synopsis Captive-fired Testing of Solid Rocket Motors by : James W. Kordig
Download or read book Captive-fired Testing of Solid Rocket Motors written by James W. Kordig and published by . This book was released on 1971 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Study of Combustion and Flow Behaviour in Solid-propellant Rocket Motors by : D. R. Greatrix
Download or read book A Study of Combustion and Flow Behaviour in Solid-propellant Rocket Motors written by D. R. Greatrix and published by . This book was released on 1987 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Characterization of Rocket Propellant Combustion Products. (Description of Sampling and Analysis Methods for Rocket Exhaust Characterization Studies). by :
Download or read book Characterization of Rocket Propellant Combustion Products. (Description of Sampling and Analysis Methods for Rocket Exhaust Characterization Studies). written by and published by . This book was released on 1990 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: This effort arose from a need of the US Army's Biomedical Research and Development Laboratory to understand potential adverse health impacts of the use of hand-held anti-tank weapon systems. An approach was developed and validated for sampled and chemical characterization of the rocket motor exhaust generated from the firing of scaled down test motors. Major exhaust constituents were sampled and analyzed and, in near real time while performing off-site analyses, samples were collected for determination of trace constituents of the particulate and vapor phases. Interfaces studies were performed using atmospheric pressure burns of 1g quantities of propellants. Carbon monoxide and carbon dioxide were determined using non-dispersive infrared instrumentation. Airborne particulate mass concentration was determined using infrared forward scattering measurements, a tapered element oscillating microbalance, and conventional gravimetry. Particulate phase metals were determined using Teflon membrane filters, followed by inductively coupled plasma and atomic absorption analysis. Particulate phase polynuclear aromatic hydrocarbons (PAH) and nitro- PAH were collected on a two stage filter. Target species wre extracted, and quantified by gas chromatography/mass spectrometry (GC/MS). Vapor phase species were collected on multi-sorbent resin traps, and subjected to thermal desorption GC/MS. Keywords: Rocket propellants; Vapor phases; Rocket exhaust; Toxic hazards; Chemical analysis.
Book Synopsis Research on Ablative Plastic Characterization in Simulated Motor Exhaust by : S. L. Ostrow
Download or read book Research on Ablative Plastic Characterization in Simulated Motor Exhaust written by S. L. Ostrow and published by . This book was released on 1967 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt: New chemical compositions and physical constructions of ablative materials were exposed in three rocket motor combustion-gas environments to determine the potential usefulness of these materials for hyperenvironmental conditions associated with current and future solid and liquid propellant motors. These gas environments were: (1) the exhaust from a high-temperature Aeronutronic solid propellant rocket motor simulator, a nitrogen tetroxide (N2O4)-50 percent hydrazine and 50 percent unsymmetrical dimethylyhydrazine (50-50) liquid propellant environment, and a chlorine trifluoride (CTF)-hydrazine (N2H4) liquid propellant environment. Material erosion and thermal insulation characteristics of the research nozzles were evaluated by comparisons of chamber pressure versus time data, erosion and resin degradation rates, and visual photographic data. Eight nozzle specimens, comprising test series 1, were exposed to the exhaust environment of a storable liquid propellant rocket motor utilizing N2O4/50-50 at a chamber pressure of 700 psia. Twenty-five nozzle specimens (comprising test series 2) were exposed to the exhaust environment of a simulated solid propellant at a chamber pressure of 500 psia; flame temperature was 5800 F and the propellant was highly aluminized. Eight nozzle specimens, comprising test series 3, were exposed to the exhaust environment of another storable liquid propellant rocket motor utilizing CTF/N2H4 at a chamber pressure of 500 psia.
Book Synopsis Solid Propellant Chemistry Combustion and Motor Interior Ballistics 1999 by : Vigor Yang
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:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt: