USAF Propellant Handbooks. Nitric Acid/Nitrogen Tetroxide Oxidizers PDF Download
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Author: Publisher: ISBN: Category : Languages : en Pages : 207
Book Description
The Nitric Acid/Nitrogen Tetroxide Oxidizer Handbook is a compilation of engineering information on the physical and chemical properties, storage and handling, production, transportation, safety, and material compatibility of the nitric acid/nitrogen tetroxide family of oxidizers and their blends. It contains information on the following propellants: Nitric Acid (IRFNA), High Density Acid, Nitrogen Tetroxide, MON-1, MON-3, MON-10, MON-25, Minuteman Grade N2O4. The propellant handbook is intended to be used for R and D personnel and test engineers who are directly involved in the utilization of liquid rocket propellants and the design of liquid rocket propulsion systems and facilities. (Author).
Author: Publisher: ISBN: Category : Languages : en Pages : 207
Book Description
The Nitric Acid/Nitrogen Tetroxide Oxidizer Handbook is a compilation of engineering information on the physical and chemical properties, storage and handling, production, transportation, safety, and material compatibility of the nitric acid/nitrogen tetroxide family of oxidizers and their blends. It contains information on the following propellants: Nitric Acid (IRFNA), High Density Acid, Nitrogen Tetroxide, MON-1, MON-3, MON-10, MON-25, Minuteman Grade N2O4. The propellant handbook is intended to be used for R and D personnel and test engineers who are directly involved in the utilization of liquid rocket propellants and the design of liquid rocket propulsion systems and facilities. (Author).
Author: Vigor Young Publisher: AIAA ISBN: 9781600864186 Category : Liquid propellant rockets Languages : en Pages : 606
Book Description
Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Author: Stephen D. Heister Publisher: Cambridge University Press ISBN: 1108395066 Category : Technology & Engineering Languages : en Pages : 589
Book Description
A modern pedagogical treatment of the latest industry trends in rocket propulsion, developed from the authors' extensive experience in both industry and academia. Students are guided along a step-by-step journey through modern rocket propulsion, beginning with the historical context and an introduction to top-level performance measures, and progressing on to in-depth discussions of the chemical aspects of fluid flow combustion thermochemistry and chemical equilibrium, solid, liquid, and hybrid rocket propellants, mission requirements, and an overview of electric propulsion. With a wealth of homework problems (and a solutions manual for instructors online), real-life case studies and examples throughout, and an appendix detailing key numerical methods and links to additional online resources, this is a must-have guide for senior and first year graduate students looking to gain a thorough understanding of the topic along with practical tools that can be applied in industry.
Author: Russell Wanhill Publisher: Springer ISBN: 3319895303 Category : Technology & Engineering Languages : en Pages : 73
Book Description
This SpringerBrief discusses the determination and classification of the ambient temperature corrosion and stress corrosion properties of aerospace structural alloys, with emphasis on (1) aluminium alloys, modern (3rd generation) aluminium‒lithium alloys, stainless steels and titanium alloys and (2) some of the issues involved. Standard /reference data on environmental properties, including corrosion and stress corrosion, are mandatory for the qualification and certification of materials for aerospace vehicles, and also for the design of actual structures and components. Recommendations for further testing and evaluation are given at appropriate points in the text. The book concludes with a summary of the main topics.
Author: Ashley Chandler Karp Publisher: Academic Press ISBN: 0128165936 Category : Technology & Engineering Languages : en Pages : 344
Book Description
Hybrid Rocket Propulsion Design Handbook provides system scaling laws, design methodologies, and a summary of available test data, giving engineers all the tools they need to develop realistic hybrid system designs.Important supporting theory from chemistry, thermodynamics, and rocket propulsion is addressed, helping readers from a variety of backgrounds to understand this interdisciplinary subject. This book also suggests guidelines for standardized reporting of test data, in response to difficulties researchers have in working with results from different research institutes. - Covers general theory, recent advances and current fragmented experimental results of hybrid rocket engines - Outlines testing standards for hybrid researchers - Provides guidance on how to use a freely available online code from NASA
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Author: Alfred C. Wright
Author: Mohammed Habiballah
Author: Vigor Young
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Author: Stephen D. Heister
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Author: Ashley Chandler Karp
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