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
      Armor
      Spacecraft Trajectories and Reentry

Distribution Statement : APPROVED FOR PUBLIC RELEASE