Accession Number : AD0780834

Title :   Solid-Propellant Rocket Engines,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Vinitskii,A. M.

Report Date : 09 APR 1974

Pagination or Media Count : 454

Abstract : The book describes the motion of combustion products in the chamber and nozzle of solid-propellant rocket engine. The spreads of intrachamber and output characteristics of RDTT, caused by random and systematic deviations of the loading parameters are analyzed. The effect of the engine and propellant characteristics on the ideal velocity of the rocket is also analyzed. The book also examines the procedure for profiling of nozzles, the motion of two-phase combustion products, and the calculation and design of charges from solid rocket propellants.

Descriptors :   *Solid propellant rocket engines, Translations, Equations of motion, Combustion chambers, Combustion products, Solid rocket propellants, Rocket nozzles, Thrust, Interior ballistics, Gas dynamics, USSR

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE