This second edition of the classic on the thermochemistry of combustion now features five new chapters and updated coverage of significant recent developments in the field. Addressing both experimental as well as theoretical aspects, the book covers the thermochemical and combustion characteristics of all important types of energetic materials, such as explosives, propellants, and the new class of pyrolants, as well as related phenomena. It presents the fundamental bases of the energetics of materials, deflagration and detonation, thermochemical process of decomposition and combustion, plus combustion wave structures. The book also goes on to discuss the combustion mechanisms of various types of energetic materials, propellants, and explosives, based on the heat transfer process in the combustion waves. The burning rate models are also presented as an aid to understanding the rate-controlling steps of combustion processes, thus demonstrating the relationships of burning rate versus pressure and initial temperature. As a major topic new to this edition, new propulsion methods such as duct rockets, ramjets, pulse motors and thrusters are described in detail, while appendices on flow field dynamics and shock wave propagation have been added.
About the Author
Dr. Kubota received a Doctorate from Princeton University in 1973, majoring in "Solid Propellant Combustion" and "Rocket Propulsion including Ducted Rocket Engine". His current position is Senior Research Scientist of Propellant Combustion Laboratory, Asahi Kasei Chemicals. Previously, he was Director, Third Research Center, Technical Research and Development Institute (TRDI), Japan Defense Agency, which is responsible for aircraft and missiles.
New to Edition
Newly developed propulsion systems such as ducted rockets, pulse motors and impulse thrusters as well as pyrolants, a new class of materials, are covered in detail. The original nine chapters have been completely revised and another six have been added: Formation of Energetic Pyrolants, Combustion Propagation of Pyrolants, Emission from Combustion Products, Transient Combustion, Rocket Thrust Modulation, and Ducted Rocket Propulsion. New appendices on flow field dynamics and shock wave propagation have been added.
