Accession Number : AD0706663

Title :   FLIGHT DYNAMICS: TRAJECTORIES OF FLIGHT VEHICLES (SELECTED PARTS),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Ostoslavskii, I. V. ; Strazheva, I. V.

Report Date : 02 FEB 1970

Pagination or Media Count : 34

Abstract : In addition to the Annotation of the forewords to the first and second edition, the translation encompasses sections of the monograph dealing with the theoretical flight dynamics of three dimensional maneuvers and the calculation of the trajectory of a winged rocket aircraft. Calculation equations are given for the chandelle; only brief descriptions are given of the half roll, Immelmann, and roll. Extensive mathematical treatment of the behavior of a rocket powered winged vehicle in the atmosphere is presented from the point of view of the variational problem of the optimum flight program. (Author)

Descriptors :   *ROCKET AIRCRAFT, *FLIGHT PATHS, ROLL, OPTIMIZATION, LIFT, USSR.

Subject Categories : Research and Experimental Aircraft
      Military Aircraft Operations

Distribution Statement : APPROVED FOR PUBLIC RELEASE