Accession Number : AD0717820

Title :   Dynamics Missiles,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Abgaryan,K. A. ; Rapoport,I. M.

Report Date : 06 NOV 1970

Pagination or Media Count : 502

Abstract : In the book are discussed fundamentals of dynamics of rocket operating on solid and liquid propellants. There are listed equations of undisturbed and disturbed motion of rockets as bodies of variable composition, methods of linearization of equations and decomposition of linearized equations into separate groups. There are examined stability and controllability of the rocket, its transfer functions and dynamic characteristics as the object of control. There are comprehensively examined questions of stabilization of the rocket taking into account the elasticity of its construction and mobility of liquid propellant in the tanks. The book is intended for students of engineering colleges and can be useful for engineers of the aviation and rocket industry. (Author)

Descriptors :   (*GUIDED MISSILES, DYNAMICS), SOLID PROPELLANT ROCKET ENGINES, LIQUID PROPELLANT ROCKET ENGINES, GUIDED MISSILE TRAJECTORIES, STABILITY, PROPELLANT TANKS, SLOSHING, EQUATIONS OF MOTION, USSR

Subject Categories : Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE