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  Testing LISA drag-free control with the LISA technology package flight experiment

Bortoluzzi, D., Bosetti, P., Carbone, L., Cavalleri, A., Ciccolella, A., Da Lio, M., et al. (2003). Testing LISA drag-free control with the LISA technology package flight experiment. Classical and Quantum Gravity, 20(10), S89-S97. doi:10.1088/0264-9381/20/10/311.

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Item Permalink: http://hdl.handle.net/11858/00-001M-0000-0013-52A9-4 Version Permalink: http://hdl.handle.net/11858/00-001M-0000-0013-52AA-2
Genre: Journal Article

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23742.pdf (Publisher version), 147KB
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Bortoluzzi, D., Author
Bosetti, P., Author
Carbone, L., Author
Cavalleri, A., Author
Ciccolella, A., Author
Da Lio, M., Author
Danzmann, Karsten1, Author              
Dolesi, R., Author
Gianolio, Alberto, Author
Heinzel, Gerhard1, Author              
Hoyland, D., Author
Hoyle, D., Author
Hueller, M., Author
Nappo, F., Author
Sallusti, M., Author
Sarra, P., Author
te Plate, M., Author
Tirabassi, C., Author
Vitale, S., Author
Weber, W. J., Author
Affiliations:
1Laser Interferometry & Gravitational Wave Astronomy, AEI-Hannover, MPI for Gravitational Physics, Max Planck Society, escidoc:24010              

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 Abstract: The LISA test masses must be kept free of stray acceleration noise to within 3 × 10-15 m s-2 Hz-1/2 in order to obtain the low-frequency gravitational wave sensitivity goal. The LISA technology package (LTP) is a dedicated ESA flight experiment for testing the drag-free control technology that must ensure purity of free fall in the LISA mission. We present here a brief description of the LTP experimental configuration, specific measurements to be performed and the requirements that must be met in order to demonstrate the LTP stray acceleration upper limit goal of 3 × 10-14 m s-2 Hz-1/2 at 1 mHz.

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Language(s): eng - English
 Dates: 2003
 Publication Status: Published in print
 Pages: -
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 Rev. Method: -
 Identifiers: eDoc: 23742
DOI: 10.1088/0264-9381/20/10/311
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Title: Classical and Quantum Gravity
Source Genre: Journal
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Pages: - Volume / Issue: 20 (10) Sequence Number: - Start / End Page: S89 - S97 Identifier: ISSN: 0264-9381