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Hybrid Rocket Propulsion Design Handbook

Hybrid Rocket Propulsion Design Handbook
Author: Ashley Chandler Karp
Publisher: Academic Press
Total Pages: 344
Release: 2023-10-07
Genre: Technology & Engineering
ISBN: 0128165936

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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


The Science and Design of the Hybrid Rocket Engine

The Science and Design of the Hybrid Rocket Engine
Author: Richard M Newlands
Publisher:
Total Pages: 0
Release: 2017-04-21
Genre: Rocket engines
ISBN: 9780244600525

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This is a textbook about rocket engineering, concentrating on the nitrous oxide hybrid rocket engine, both small and large. It's also a book about the science of chemical rockets in detail: three of the chapters are full of in-depth rocket science describing how all chemical rockets work. After a first chapter brushing up on the science and maths you'll need, the book describes the choice and safe use of hybrid rocket propellants, and how they're handled in practice. Then there are the rocket science chapters. Then you learn how to design, construct, and operate, a large hybrid rocket engine capable of getting you into Space. The book also includes a practical guide to the testing of hybrid rocket engines large and small, and how to fly them safely. Included are full instructions for programming a rocket trajectory simulator in Microsoft Excel, and several appendices containing rocketry information and equations, and instructions on how to design a bell nozzle.


Advances in Hybrid Rocket Technology and Related Analysis Methodologies

Advances in Hybrid Rocket Technology and Related Analysis Methodologies
Author: Carmine Carmicino
Publisher: MDPI
Total Pages: 352
Release: 2020-12-07
Genre: Technology & Engineering
ISBN: 3039433903

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The book is an amazing collection of technical papers dealing with hybrid rockets. Once perceived as a niche technology, for about a decade, hybrid rockets have enjoyed renewed interest from both the propulsion technical community and industry. Hybrid motors can be used in practically all applications where a rocket is employed, but there are certain cases where they present a superior fit, such as sounding rockets, tactical missile systems, launch boosters and the emerging field of commercial space transportation. The novel space tourism business, indeed, will benefit from their safety and lower recurrent development costs. The subjects addressed in the book include the cutting edge technology employed to push forward this relatively new propulsion concept, spanning systems to improve fuel regression rate, control of the mixture ratio to optimize performance, computational fluid dynamics applied to the simulation of the internal ballistics, and some other novel system applications.


An Introduction to Hybrid Rockets

An Introduction to Hybrid Rockets
Author:
Publisher:
Total Pages:
Release:
Genre:
ISBN:

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Discusses the potential advantages of developing a "hybrid" rocket motor for use in space vehicle propulsion. Also announces a group has been formed at the University of Illinois to design and test a test-scale hybrid rocket motor. Describes the advanatages and disadvatages of current rocket propulsion systems. Hybrid rocket motor systems mix solid fuels with fluid oxidizers.


Rocket Propulsion Elements

Rocket Propulsion Elements
Author: George P. Sutton
Publisher: John Wiley & Sons
Total Pages: 657
Release: 2011-09-09
Genre: Science
ISBN: 1118174208

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The definitive text on rocket propulsion—now revised to reflect advancements in the field For sixty years, Sutton's Rocket Propulsion Elements has been regarded as the single most authoritative sourcebook on rocket propulsion technology. As with the previous edition, coauthored with Oscar Biblarz, the Eighth Edition of Rocket Propulsion Elements offers a thorough introduction to basic principles of rocket propulsion for guided missiles, space flight, or satellite flight. It describes the physical mechanisms and designs for various types of rockets' and provides an understanding of how rocket propulsion is applied to flying vehicles. Updated and strengthened throughout, the Eighth Edition explores: The fundamentals of rocket propulsion, its essential technologies, and its key design rationale The various types of rocket propulsion systems, physical phenomena, and essential relationships The latest advances in the field such as changes in materials, systems design, propellants, applications, and manufacturing technologies, with a separate new chapter devoted to turbopumps Liquid propellant rocket engines and solid propellant rocket motors, the two most prevalent of the rocket propulsion systems, with in-depth consideration of advances in hybrid rockets and electrical space propulsion Comprehensive and coherently organized, this seminal text guides readers evenhandedly through the complex factors that shape rocket propulsion, with both theory and practical design considerations. Professional engineers in the aerospace and defense industries as well as students in mechanical and aerospace engineering will find this updated classic indispensable for its scope of coverage and utility.


Rocket Propulsion

Rocket Propulsion
Author: Stephen D. Heister
Publisher: Cambridge University Press
Total Pages: 589
Release: 2019-02-07
Genre: Technology & Engineering
ISBN: 1108395066

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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.


Design, Construction and Tests of a Rocket Propulsion Motor with Hybrid Propellant in a Static Bank

Design, Construction and Tests of a Rocket Propulsion Motor with Hybrid Propellant in a Static Bank
Author: Laura Alejandra Arteaga Moreno
Publisher:
Total Pages:
Release: 2018
Genre:
ISBN:

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The degree project arises from the interest in hybrid rocket engines since it is a modern global technology among rocket engines, and has not been built or tested in Colombia. The main objective of the project is to design, build and test a Design, build and test a 250 N hybrid thrust rocket motor. For this, the motor was designed with paraffin as the solid fuel, and nitrous oxide as the liquid oxidant when designing a methodology for design, construction and testing. In the conceptual design stage, different input parameters were defined, in which the pressure of the combustion chamber was 290 psi, nozzle temperature of 2856 K, flight time of 5 seconds, specific impulse of 185 seconds, with which the different elements of the combustion chamber could be designed, including the nozzle. Additionally, the oxidant tank and the valves system were designed for their subsequent manufacture and purchase, respectively. At the same time, the electronic system was proposed in order to measure the thrust, pressure in the combustion chamber and temperature in the nozzle; and the UCAND-3 benching test was redesigned to carry out the experiments, which were planned with a sample of three fuel grains. However, it was found that the igniter did not burn completely in any test to make the reaction between fuel and oxidant be carried out satisfactorily because the burning surface area was not enough for the reaction to take place, so it is necessary to change the ignition system. However, both the hybrid rocket engine and the benching test are ready to be used in the near future.