
Accession Number : AD0714728
Title : Thermodynamic and Ballistic Design Fundamentals of SolidPropellant Rocket Engines (Selected Chapters),
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHTPATTERSON AFB OHIO
Personal Author(s) : Orlov,B. V. ; Mazing,G. Yu.
Report Date : 02 SEP 1970
Pagination or Media Count : 242
Abstract : The book gives an account of thermodynamic principles of the calculation of solidpropellant rocket engines, engineering methods of the calculation of processes of heat exchange, principles of the theory of the combustion of solid propellants and the calculation of the indicating pressure curve in the combustion chamber of an engine. Basic information is given concerning solid rocket propellants and heatproof coverings used in solidpropellant rocket engines. Thrust control in these rocket engines with respect to magnitude and direction and also the general method of ballistic design of solidpropellant rockets are discussed. The solution of simplified problems of interior ballistics of classical artillery and recoilless weapons is covered, and a solution is given for three expressions of the law of the combustion of the solid propellant. (Author)
Descriptors : (*SOLID PROPELLANT ROCKET ENGINES, INTERIOR BALLISTICS), SOLID ROCKET PROPELLANTS, COMBUSTION, NOZZLE GAS FLOW, THERMODYNAMICS, COMBUSTION CHAMBERS, ROCKET NOZZLES, USSR
Subject Categories : Combustion and Ignition
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE