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Author : L.E. Bollinger
Publisher : Elsevier
Page : 699 pages
File Size : 13,10 MB
Release : 2013-04-22
Category : Science
ISBN : 0323163335
Liquid Rocket and Propellants
Author : Dieter K. Huzel
Publisher : AIAA
Page : 452 pages
File Size : 37,50 MB
Release : 1992
Category : Liquid propellant rocket engines
ISBN : 9781600864001
Author : George Paul Sutton
Publisher : AIAA
Page : 936 pages
File Size : 28,77 MB
Release : 2006
Category : Technology & Engineering
ISBN : 9781563476495
Liquid propellant rocket engines have propelled all the manned space flights, all the space vehicles flying to the planets or deep space, virtually all satellites, and the majority of medium range or intercontinental range ballistic missiles.
Author : Alessandro de Iaco Veris
Publisher : Springer Nature
Page : 747 pages
File Size : 13,78 MB
Release : 2020-09-26
Category : Technology & Engineering
ISBN : 3030547043
This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.
Author : John Drury Clark
Publisher : Rutgers University Press
Page : 217 pages
File Size : 49,11 MB
Release : 2018-05-23
Category : Biography & Autobiography
ISBN : 0813599199
This newly reissued debut book in the Rutgers University Press Classics Imprint is the story of the search for a rocket propellant which could be trusted to take man into space. This search was a hazardous enterprise carried out by rival labs who worked against the known laws of nature, with no guarantee of success or safety. Acclaimed scientist and sci-fi author John Drury Clark writes with irreverent and eyewitness immediacy about the development of the explosive fuels strong enough to negate the relentless restraints of gravity. The resulting volume is as much a memoir as a work of history, sharing a behind-the-scenes view of an enterprise which eventually took men to the moon, missiles to the planets, and satellites to outer space. A classic work in the history of science, and described as “a good book on rocket stuff…that’s a really fun one” by SpaceX founder Elon Musk, readers will want to get their hands on this influential classic, available for the first time in decades.
Author : David Altman
Publisher : Princeton University Press
Page : 197 pages
File Size : 37,70 MB
Release : 2015-12-08
Category : Science
ISBN : 1400879957
David Altman, James M. Carter, S. S. Penner, Martin Summerfield. High Temperature Equilibrium, Expansion Processes, Combustion of Liquid Propellants, The Liquid Propellants Rocket Engine. Originally published in 1960. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : Martin Summerfield
Publisher : Elsevier
Page : 713 pages
File Size : 45,88 MB
Release : 2013-11-11
Category : Science
ISBN : 0323163351
Solid Propellant Rocket Research
Author : David T. Harrje
Publisher :
Page : 674 pages
File Size : 21,84 MB
Release : 1972
Category : Liquid propellant rockets
ISBN :
The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.
Author : Stephen D. Heister
Publisher : Cambridge University Press
Page : 589 pages
File Size : 17,29 MB
Release : 2019-02-07
Category : Science
ISBN : 1108422276
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.
Author : Mohammad Hossein Keshavarz
Publisher :
Page : 0 pages
File Size : 32,45 MB
Release : 2018
Category : Jet planes
ISBN : 9781536143119
In recent years, it has been important for scientists and chemical industries to introduce and develop new liquid fuels as jet fuels and propellants for propulsion purposes. Different aspects should be considered for the selection of a good candidate such as combustion performance, desired physical properties, noncarcinogenic and less toxicity. New synthetic hydrocarbon fuels with favorable combustion performance and physical properties have been considered as desirable jet fuels. They can be used in aircrafts such as military jets because of their higher volumetric energy density. A liquid-propellant rocket uses liquid propellants for propulsion. Liquid propellants should have the desirable properties of high energy density per unit mass, high specific impulse, and short ignition delays. Hypergolic propellants as important classes of liquid propellants are characterized by spontaneous reaction upon fuel and oxidizer mixing and high energy yield. Moreover, they should be relatively ignitable and have a small ignition time delay. This book reviews some efforts that have been done to introduce new candidates to replace conventional hydrazine fuels because they are acutely toxic and suspected carcinogens, costly safety precautions and handling procedures are required. This book reviews the latest advances in liquid fuels, which may be used as jet fuels and liquid propellants. Important properties for assessment of a suitable liquid are demonstrated. This book can be used for graduate students in the field of chemistry and chemical engineering. It may also be useful for scientists and researchers who work on the development of new liquid fuels with high performance as well as those that are noncarcinogenic or have less toxicity.