Dynamics of the Design of a Flight Vehicle
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 05, 1970
- Accession Number
- AD0712822
Entities
People
- V. F. Gladkii
Organizations
- Air Force Systems Command