Thursday, March 21, 2013

PDF Ebook Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh

PDF Ebook Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh

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Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh

Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh


Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh


PDF Ebook Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh

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Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh

Détails sur le produit

Broché: 766 pages

Editeur : Springer-Verlag Berlin and Heidelberg GmbH & Co. K; Édition : Softcover reprint of the original 1st ed. 1968 (1 janvier 1968)

Collection : Applied Physics and Engineering

Langue : Anglais

ISBN-10: 3642461115

ISBN-13: 978-3642461118

Dimensions du produit:

15,5 x 4,5 x 23,5 cm

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Classement des meilleures ventes d'Amazon:

358.489 en Livres (Voir les 100 premiers en Livres)

This is a excellent and exhaustive text about aerospace propulsion, both air breathing and rocket systems. Unfortunately, this book seems relatively unknown and underappreciated. There are many important contributors to the text, to name a few; Antonio Ferri, George P. Sutton, Martin Summerfield, Howard Seifert, Krafft Ehricke, G.L. Dugger. Aerospace enthusiasts may recognize some of them. For example, Ferri is a prominent aerodynamicist, Summerfield is a leading specialist in solid rocket propellant and Ehricke is a famous German rocket scientist. This is an advanced text and some parts are difficult. Also, I want to mention that the book begin with an extensive review on aerodynamics and thermodynamics, an important shortcoming in Rocket Propulsion Element, the classic reference text about space propulsion.Here is the contents of the bookChapter 1. Fundamentals of Thermodynamics and AerodynamicsChapter 2. Thermodynamic Cycle Analysis of Gas Turbines and Air·breathing Propulsion SystemsChapter 3. Aerodynamic Design of Axial Flow Compressors and TurbinesChapter 4. Ramjets and Air-Augmented RocketsChapter 5. Rocket Classifications, Liquid Propellant Rockets,Engine Selection, and Heat TransfeChapter 6. Solid Propellant RocketsChapter 7. Hybrid Rocket Theory and DesignChapter 8. Nuclear Rocket PrqpulsionChapter 9. Radioisotope PropulsionChapter 10. Electric and Ion PropulsionChapter 11. Ion PropulsionChapter 12. Interaction Flows Due to Supersonic Secondary JetsChapter 13. Gasdynamics of ExplosionsChapter 14. Supersonic Combustion TechnologyChapter 15. Combustion Instability TheoryChapter 16. An Advanced Space Propulsion ConceptChapter 17. Zero 9 Propulsion ProblemsChapter 18. Propulsion Systems-Comparison and Evaluation for Space Missions

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Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh PDF
Jet, Rocket, Nuclear, Ion and Electric Propulsion: Theory and Design, by W. H. T. Loh PDF

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