Accession Number : AD0720739
Title : Rocket Flight Theory,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Vorobev,L. M.
Report Date : 19 JAN 1971
Pagination or Media Count : 259
Abstract : The book is devoted to the flight dynamics of a rocket in its powered phase. Particular attention is devoted to an examination of analytical methods of obtaining the characteristics of the motion of the center of mass of an airborne vehicle.
Descriptors : (*ROCKET TRAJECTORIES, EQUATIONS OF MOTION), (*GUIDED MISSILE TRAJECTORIES, EQUATIONS OF MOTION), DYNAMICS, KINEMATICS, AERODYNAMICS, DIFFERENTIAL EQUATIONS, INTEGRALS, NUMERICAL INTEGRATION, BESSEL FUNCTIONS, INEQUALITIES, SEQUENCES(MATHEMATICS), CONVERGENCE, DYNAMIC PROGRAMMING, LAUNCH VEHICLES, OPTIMIZATION, USSR
Subject Categories : Guided Missile Dynam, Config & Cntrl Surfaces
Spacecraft Trajectories and Reentry
Distribution Statement : APPROVED FOR PUBLIC RELEASE