Staged Combustion Hybrid Rocket Test Facility Design PDF Download

Author: Ryuichi Sekita
Publisher:
ISBN:
Category : Hybrid propellant rockets
Languages : en
Pages : 186

View

Book Description

Author: Ashley Chandler Karp
Publisher: Academic Press
ISBN: 0128165936
Category : Technology & Engineering
Languages : en
Pages : 344

View

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

Author: Nathan W. H. Smith
Publisher:
ISBN:
Category :
Languages : en
Pages :

View

Book Description

Author:
Publisher:
ISBN: 9781563477034
Category : Aeronautics
Languages : en
Pages : 648

View

Book Description

Author: Joshua Gardner
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 80

View

Book Description

Author: Dieter K. Huzel
Publisher: AIAA
ISBN: 9781600864001
Category : Liquid propellant rocket engines
Languages : en
Pages : 452

View

Book Description

Author: Laura Alejandra Arteaga Moreno
Publisher:
ISBN:
Category :
Languages : en
Pages :

View

Book Description
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.

Author: Ronald Humble
Publisher: Learning Solutions
ISBN: 9780070313200
Category : Technology & Engineering
Languages : en
Pages : 0

View

Book Description
The only comprehensive text available on space propulsion for students and professionals in astronautics.

Author: DP Mishra
Publisher: CRC Press
ISBN: 1351708414
Category : Technology & Engineering
Languages : en
Pages : 364

View

Book Description
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.

Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 36

View

Book Description