An attempt is made to indicate the research studies which should be vigorously supported in order to provide necessary information for the solution of structural dynamic problems of missile and space vehicles. The problem areas are discussed in terms of the disciplines or functions required in their solution. Among the latter are: (1) interactions of the complete system and the environment, (2) criteria for design conditions and performance, (3) interactions of aerodynamic forces with flexible structures, (4) motion of liquids, (5) vibration, (6) impulsive loading and transient responses, (7) guidance and control, (8) testing, and (9) materials considerations. In addition, some correlation is provided for identifying the problems in terms of the environmental conditions in which they occur.
Important Research Problems in Missile and Spacecraft Structural Dynamics, 1961
01.05.1962
Sonstige
Keine Angabe
Englisch
Spacecraft and missile test discipline
AIAA | 1981
|International missile and spacecraft guide
TIBKAT | 1960
|