Accession Number : AD0712822

Title :   DYNAMICS OF THE DESIGN OF A FLIGHT VEHICLE,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Gladkii,V. F.

Report Date : 05 AUG 1970

Pagination or Media Count : 301

Abstract : The book is devoted to the problem of determining the necessary carrying capacity and rigidity of design of a flight vehicle. Discussed in it are theoretical bases and practical methods of the calculation of internal force factors from external forces acting on the vehicle in the process of operation, and methods of development of calculation cases of loading are given. In this case the main attention is given to problems of the dynamics of design, in particular the selection of design configurations, the formulation of equations of dynamic equilibrium and determination of the dynamic reaction of design on the effect of external perturbations. Consideration is given to those limitations which are imposed by conditions of strength of the design on values of certain parameters of the propulsion system, automatic control system, complex of ground equipment, and also on conditions of operation of flight vehicles of different types. (Author)

Descriptors :   (*GUIDED MISSILES, DESIGN), (*SPACECRAFT, DESIGN), (*AIRCRAFT, DESIGN), AERODYNAMIC LOADING, PROPULSION SYSTEMS, CONTROL SYSTEMS, GROUND SUPPORT EQUIPMENT, USSR

Subject Categories : Aircraft
      Guided Missiles
      Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE