Most of the structural dynamics resources allocated to the Space Shuttle are concentrated on the flight events which result in critical structural loads and/or minimum control stability margins. Since these events are primarily sub-orbital, the data base of interest to those involved in orbital experimentation is somewhat limited. A brief discussion of available data is given. Although estimates of peak acceleration levels and the associated frequency spectrum in the payload bay due to thrusting of the various control system thrusters were made, the actual levels and time histories must be based on updated structural math models and a detailed knowledge of the input forcing functions.
Elastic body dynamics
1981-11-01
Conference paper
No indication
English
Simulation of Driveline Rattle using Elastic Multi Body Dynamics Approach
British Library Conference Proceedings | 2017
|Simulation of Driveline Rattle using Elastic Multi Body Dynamics Approach
SAE Technical Papers | 2017
|