Solid Rocket Propulsion Technology
| Author | : | |
| Rating | : | 4.12 (967 Votes) |
| Asin | : | 0080409997 |
| Format Type | : | paperback |
| Number of Pages | : | 620 Pages |
| Publish Date | : | 2015-04-30 |
| Language | : | English |
DESCRIPTION:
formulas are small and can't change with zoom formulas are small and can't change with zoom. It bothers methe content is very complete. "Must have for anybody involved in ballistics" according to J. G Scott. I received this book as a gift many years ago as I made my transition from simple engineer to an analyst of CAD/PAD devices. If you are interested in propellants you can find many rare references and very good working closed form solutions. A majority of the work . musolesi luca said Finalmente delle risposte.. Finalmente un libro completo sulla propulsione a razzo a propellente solido, in 600 pagine di libro vengono trattati molti argomenti, ed in modo professionale, con metodologie molto moderne, come ad esempio l'uso di modellazioni del grano di propellente con progra
This book, a translation of the French title Technologie des Propergols Solides, offers otherwise unavailable information on the subject of solid propellants and their use in rocket propulsion. Thus the reader not only has an overall picture of solid rocket propulsion technology but a comprehensive view of its different developmental permutations worldwide.. The fundamentals of rocket propulsion are developed in chapter one and detailed descriptions of concepts are covered in the following chapters. The material used in the book has been collected from different countries, as the development of this field has occurred separately due to the classified nature of the subject. Specific design methods and the theoretical physics underlying them are presented, and finally the industrial production of the propellant itself is explained
Mark WilliamsonThis book provides an excellent review of the technology.Earth Space ReviewG.I. Evansof particular interest to readers seeking a comprehensive survey of the relationship of component technologies to rocket motor designdeal very well withrocket plume signature characteristics andhazard/vulnerability of the rocket motor to thermal and mechanical stimuli.The Aeronautical Journal