Vibro-Acoustic Diagnostic Testing Method for the Characterization and the Control of Emitted Noise on ISS ATV Manned Modules - Lessons Learned
- Paper number
IAC-07-C2.8.04
- Author
Mr. Pietro Carlo Marucchi Chierro, Alcatel Alenia Space Italia, Italy
- Coauthor
Mr. Giorgio Cabodi, Alcatel Alenia Space Italia, Italy
- Coauthor
Mr. Francesco Quagliotti, Alcatel Alenia Space Italia, Italy
- Coauthor
Mr. Nicola Riva, Italy
- Year
2007
- Abstract
On-orbit Vibro-acoustics has found exciting applications in modern manned space systems because of audible noise/human vibration requirements.
In the frame of this paper, the results of ATV Design & Verification approach vs the NC50 and the ISS Micro-g requirement are presented.
The aim of this paper is to highlight:
- the integrated Test/Analysis approach selected for the Design & Verification of the Pressurized modules
- the specific developed methods on how to characterize the disturbers I/F forcing function and their emitted acoustics for the full control of the budget contributions to the System induced Vibro-acoustic environment
- the recovery actions selection methodology and their design for compliance achievement and pleasant acoustic environment performance
- On-field diagnostic test method to find out unexpected disturbers impact for their further recovery means implementation as per ATV project.
- Diagnostic post-processing approach on measured data for the selection, Design and implementation of technical solution involving crew activities in the frame of the on orbit tasks of the passive recovery means
- Validation testing to see the effect of the implemented acoustic means
- Standardization of “Industrial procedure” for the next manned Spacecraft project generation derived from the AAS-I acquired experience for the On-orbit Vibroacoustics control in the selected Design & Verification approaches
- the sharing of the verification approach at Unit, S/S and System level to optimize test philosophy and to save cost.
- Abstract document
- Manuscript document
IAC-07-C2.8.04.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.