Vibration and Acoustic Testing for Mars Micromission Spacecraft
Unique spacecraft dynamics qualification methodologies have been developed at the Jet Propulsion Laboratory in recent years in response to NASA's faster/better/cheaper initiative.
Engineering topics
Publications and source records attributed to Kern, D..
Unique spacecraft dynamics qualification methodologies have been developed at the Jet Propulsion Laboratory in recent years in response to NASA's faster/better/cheaper initiative.
The topics are presented in viewgraph form and include: a vibroacoustic payload environment prediction system (VAPEPS); objectives of the JPL space station analysis effort; statistical energy analysis (SEA); VAPEPS Space Station Freedom (SSF) model description; noise control treatments; and SSF microgravity preliminary analysis results.
The vibration, acoustic and low frequency loads data from the first 5 shuttle flights are presented. The engineering analysis of that data is also presented. Vibroacoustic data from STS-9 are also presented because they represent the only data taken on a large payload. Payload dynamic environment predictions developed by the participation of various NASA and industrial centers are presented along with a comparison of analytical loads methodology predictions with flight data, including a brief description of the methodologies employed in developing those predictions for payloads. The review of prediction methodologies illustrates how different centers have approached the problems of developing shuttle dynamic environmental predictions and criteria. Ongoing research activities related to the shuttle dynamic environments are also described. Analytical software recently developed for the prediction of payload acoustic and vibration environments are also described.