Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures

LISA Pathfinder satellite was launched on 3 December 2015 toward the Sun–Earth first Lagrangian point (L1) where the LISA Technology Package (LTP), which is the main science payload, will be tested. LTP achieves measurements of differential acceleration of free-falling test masses (TMs) with sensiti...

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Autores: Armano, M., Audley, H., Auger, G., Baird, J., Binetruy, P., Born, M., Bortoluzzi, D., Brandt, N., Bursi, A., Caleno, M., Cavalleri, A., Cesarini, A., Cruise, M., Danzmann, K., de Deus Silva, M., Desiderio, D., Piersanti, E., Diepholz, I., Dolesi, R., Dunbar, N., Ferraioli, Luigi, Ferroni, V., Fitzsimons, E. D., Flatscher, R., Freschi, M., Gallegos, J., García Marirrodriga, C., Gerndt, R., Gesa, L., Gibert, F., Giardini, D., Giusteri, R., Grimani, C., Grzymisch, J., Harrison, I., Heinzel, G., Hewitson, M., Hollington, D., Hueller, M., Huesler, J., Inchauspé, H., Jennrich, O., Jetzer, P., Johlander, B., Karnesis, N., Kaune, B., Korsakova, N., Killow, C. J., Lloro, I., Liu, L., López Zaragoza, J. P., Maarschalkerweerd, R., Madden, S., Mance, D., Martín, V., Martín Polo, L., Martino, J., Martín Porqueras, F., Mateos, I., McNamara, P. W., Mendes, J., Mendes, L., Moroni, A., Nofrarias, M., Paczkowski, S., Perreur Lloyd, M., Petiteau, A., Pivato, P., Plagnol, E., Prat, P., Ragnit, U., Ramos Castro, J., Reiche, J., Romera Pérez, J.A., Rozemeijer, H., Rivas García, Francisco, Russano, G., Sarra, P., Schleicher, A., Slutsky, J., Sopuerta, C. F., Sumner, T., Texier, D., Thorpe, J. I., Tomlinson, R., Trenkel, C., Vetrugno, D., Vitale, S., Wanner, G., Ward, H., Warren, C., Wass, P. J., Wealthy, D., Weber, W. J., Wittchen, A., Zanoni, C., Ziegler, T., Zweifel, P.
Tipo de recurso: artículo
Fecha de publicación:2016
País:España
Institución:Universidad Loyola Andalucía
Repositorio:Brújula
OAI Identifier:oai:repositorio.uloyola.es:20.500.12412/4648
Acceso en línea:https://hdl.handle.net/20.500.12412/4648
Access Level:acceso abierto
Palabra clave:LISA
Pathfinder
Self-gravity
Differential accelerometer
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spelling Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing proceduresArmano, M.Audley, H.Auger, G.Baird, J.Binetruy, P.Born, M.Bortoluzzi, D.Brandt, N.Bursi, A.Caleno, M.Cavalleri, A.Cesarini, A.Cruise, M.Danzmann, K.de Deus Silva, M.Desiderio, D.Piersanti, E.Diepholz, I.Dolesi, R.Dunbar, N.Ferraioli, LuigiFerroni, V.Fitzsimons, E. D.Flatscher, R.Freschi, M.Gallegos, J.García Marirrodriga, C.Gerndt, R.Gesa, L.Gibert, F.Giardini, D.Giusteri, R.Grimani, C.Grzymisch, J.Harrison, I.Heinzel, G.Hewitson, M.Hollington, D.Hueller, M.Huesler, J.Inchauspé, H.Jennrich, O.Jetzer, P.Johlander, B.Karnesis, N.Kaune, B.Korsakova, N.Killow, C. J.Lloro, I.Liu, L.López Zaragoza, J. P.Maarschalkerweerd, R.Madden, S.Mance, D.Martín, V.Martín Polo, L.Martino, J.Martín Porqueras, F.Mateos, I.McNamara, P. W.Mendes, J.Mendes, L.Moroni, A.Nofrarias, M.Paczkowski, S.Perreur Lloyd, M.Petiteau, A.Pivato, P.Plagnol, E.Prat, P.Ragnit, U.Ramos Castro, J.Reiche, J.Romera Pérez, J.A.Rozemeijer, H.Rivas García, FranciscoRussano, G.Sarra, P.Schleicher, A.Slutsky, J.Sopuerta, C. F.Sumner, T.Texier, D.Thorpe, J. I.Tomlinson, R.Trenkel, C.Vetrugno, D.Vitale, S.Wanner, G.Ward, H.Warren, C.Wass, P. J.Wealthy, D.Weber, W. J.Wittchen, A.Zanoni, C.Ziegler, T.Zweifel, P.LISAPathfinderSelf-gravityDifferential accelerometerLISA Pathfinder satellite was launched on 3 December 2015 toward the Sun–Earth first Lagrangian point (L1) where the LISA Technology Package (LTP), which is the main science payload, will be tested. LTP achieves measurements of differential acceleration of free-falling test masses (TMs) with sensitivity below $3\times {10}^{-14}\,{\rm{m}}\,{{\rm{s}}}^{-2}\,{\mathrm{Hz}}^{-1/2}$ within the 1–30 mHz frequency band in one-dimension. The spacecraft itself is responsible for the dominant differential gravitational field acting on the two TMs. Such a force interaction could contribute a significant amount of noise and thus threaten the achievement of the targeted free-fall level. We prevented this by balancing the gravitational forces to the sub nm s-2 level, guided by a protocol based on measurements of the position and the mass of all parts that constitute the satellite, via finite element calculation tool estimates. In this paper, we will introduce the gravitational balance requirements and design, and then discuss our predictions for the balance that will be achieved in flight.2016info:eu-repo/semantics/articlehttps://hdl.handle.net/20.500.12412/4648reponame:Brújulainstname:Universidad Loyola AndalucíaInglésThe author acknowledges and thanks ASI and CGS for supporting this work.http://creativecommons.org/licenses/by-nc-nd/4.0/info:eu-repo/semantics/openAccessoai:repositorio.uloyola.es:20.500.12412/46482026-06-24T12:48:37Z
dc.title.none.fl_str_mv Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
title Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
spellingShingle Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
Armano, M.
LISA
Pathfinder
Self-gravity
Differential accelerometer
title_short Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
title_full Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
title_fullStr Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
title_full_unstemmed Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
title_sort Constraints on LISA pathfinder's self-gravity: design requirements, estimates and testing procedures
dc.creator.none.fl_str_mv Armano, M.
Audley, H.
Auger, G.
Baird, J.
Binetruy, P.
Born, M.
Bortoluzzi, D.
Brandt, N.
Bursi, A.
Caleno, M.
Cavalleri, A.
Cesarini, A.
Cruise, M.
Danzmann, K.
de Deus Silva, M.
Desiderio, D.
Piersanti, E.
Diepholz, I.
Dolesi, R.
Dunbar, N.
Ferraioli, Luigi
Ferroni, V.
Fitzsimons, E. D.
Flatscher, R.
Freschi, M.
Gallegos, J.
García Marirrodriga, C.
Gerndt, R.
Gesa, L.
Gibert, F.
Giardini, D.
Giusteri, R.
Grimani, C.
Grzymisch, J.
Harrison, I.
Heinzel, G.
Hewitson, M.
Hollington, D.
Hueller, M.
Huesler, J.
Inchauspé, H.
Jennrich, O.
Jetzer, P.
Johlander, B.
Karnesis, N.
Kaune, B.
Korsakova, N.
Killow, C. J.
Lloro, I.
Liu, L.
López Zaragoza, J. P.
Maarschalkerweerd, R.
Madden, S.
Mance, D.
Martín, V.
Martín Polo, L.
Martino, J.
Martín Porqueras, F.
Mateos, I.
McNamara, P. W.
Mendes, J.
Mendes, L.
Moroni, A.
Nofrarias, M.
Paczkowski, S.
Perreur Lloyd, M.
Petiteau, A.
Pivato, P.
Plagnol, E.
Prat, P.
Ragnit, U.
Ramos Castro, J.
Reiche, J.
Romera Pérez, J.A.
Rozemeijer, H.
Rivas García, Francisco
Russano, G.
Sarra, P.
Schleicher, A.
Slutsky, J.
Sopuerta, C. F.
Sumner, T.
Texier, D.
Thorpe, J. I.
Tomlinson, R.
Trenkel, C.
Vetrugno, D.
Vitale, S.
Wanner, G.
Ward, H.
Warren, C.
Wass, P. J.
Wealthy, D.
Weber, W. J.
Wittchen, A.
Zanoni, C.
Ziegler, T.
Zweifel, P.
author Armano, M.
author_facet Armano, M.
Audley, H.
Auger, G.
Baird, J.
Binetruy, P.
Born, M.
Bortoluzzi, D.
Brandt, N.
Bursi, A.
Caleno, M.
Cavalleri, A.
Cesarini, A.
Cruise, M.
Danzmann, K.
de Deus Silva, M.
Desiderio, D.
Piersanti, E.
Diepholz, I.
Dolesi, R.
Dunbar, N.
Ferraioli, Luigi
Ferroni, V.
Fitzsimons, E. D.
Flatscher, R.
Freschi, M.
Gallegos, J.
García Marirrodriga, C.
Gerndt, R.
Gesa, L.
Gibert, F.
Giardini, D.
Giusteri, R.
Grimani, C.
Grzymisch, J.
Harrison, I.
Heinzel, G.
Hewitson, M.
Hollington, D.
Hueller, M.
Huesler, J.
Inchauspé, H.
Jennrich, O.
Jetzer, P.
Johlander, B.
Karnesis, N.
Kaune, B.
Korsakova, N.
Killow, C. J.
Lloro, I.
Liu, L.
López Zaragoza, J. P.
Maarschalkerweerd, R.
Madden, S.
Mance, D.
Martín, V.
Martín Polo, L.
Martino, J.
Martín Porqueras, F.
Mateos, I.
McNamara, P. W.
Mendes, J.
Mendes, L.
Moroni, A.
Nofrarias, M.
Paczkowski, S.
Perreur Lloyd, M.
Petiteau, A.
Pivato, P.
Plagnol, E.
Prat, P.
Ragnit, U.
Ramos Castro, J.
Reiche, J.
Romera Pérez, J.A.
Rozemeijer, H.
Rivas García, Francisco
Russano, G.
Sarra, P.
Schleicher, A.
Slutsky, J.
Sopuerta, C. F.
Sumner, T.
Texier, D.
Thorpe, J. I.
Tomlinson, R.
Trenkel, C.
Vetrugno, D.
Vitale, S.
Wanner, G.
Ward, H.
Warren, C.
Wass, P. J.
Wealthy, D.
Weber, W. J.
Wittchen, A.
Zanoni, C.
Ziegler, T.
Zweifel, P.
author_role author
author2 Audley, H.
Auger, G.
Baird, J.
Binetruy, P.
Born, M.
Bortoluzzi, D.
Brandt, N.
Bursi, A.
Caleno, M.
Cavalleri, A.
Cesarini, A.
Cruise, M.
Danzmann, K.
de Deus Silva, M.
Desiderio, D.
Piersanti, E.
Diepholz, I.
Dolesi, R.
Dunbar, N.
Ferraioli, Luigi
Ferroni, V.
Fitzsimons, E. D.
Flatscher, R.
Freschi, M.
Gallegos, J.
García Marirrodriga, C.
Gerndt, R.
Gesa, L.
Gibert, F.
Giardini, D.
Giusteri, R.
Grimani, C.
Grzymisch, J.
Harrison, I.
Heinzel, G.
Hewitson, M.
Hollington, D.
Hueller, M.
Huesler, J.
Inchauspé, H.
Jennrich, O.
Jetzer, P.
Johlander, B.
Karnesis, N.
Kaune, B.
Korsakova, N.
Killow, C. J.
Lloro, I.
Liu, L.
López Zaragoza, J. P.
Maarschalkerweerd, R.
Madden, S.
Mance, D.
Martín, V.
Martín Polo, L.
Martino, J.
Martín Porqueras, F.
Mateos, I.
McNamara, P. W.
Mendes, J.
Mendes, L.
Moroni, A.
Nofrarias, M.
Paczkowski, S.
Perreur Lloyd, M.
Petiteau, A.
Pivato, P.
Plagnol, E.
Prat, P.
Ragnit, U.
Ramos Castro, J.
Reiche, J.
Romera Pérez, J.A.
Rozemeijer, H.
Rivas García, Francisco
Russano, G.
Sarra, P.
Schleicher, A.
Slutsky, J.
Sopuerta, C. F.
Sumner, T.
Texier, D.
Thorpe, J. I.
Tomlinson, R.
Trenkel, C.
Vetrugno, D.
Vitale, S.
Wanner, G.
Ward, H.
Warren, C.
Wass, P. J.
Wealthy, D.
Weber, W. J.
Wittchen, A.
Zanoni, C.
Ziegler, T.
Zweifel, P.
author2_role author
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dc.subject.none.fl_str_mv LISA
Pathfinder
Self-gravity
Differential accelerometer
topic LISA
Pathfinder
Self-gravity
Differential accelerometer
description LISA Pathfinder satellite was launched on 3 December 2015 toward the Sun–Earth first Lagrangian point (L1) where the LISA Technology Package (LTP), which is the main science payload, will be tested. LTP achieves measurements of differential acceleration of free-falling test masses (TMs) with sensitivity below $3\times {10}^{-14}\,{\rm{m}}\,{{\rm{s}}}^{-2}\,{\mathrm{Hz}}^{-1/2}$ within the 1–30 mHz frequency band in one-dimension. The spacecraft itself is responsible for the dominant differential gravitational field acting on the two TMs. Such a force interaction could contribute a significant amount of noise and thus threaten the achievement of the targeted free-fall level. We prevented this by balancing the gravitational forces to the sub nm s-2 level, guided by a protocol based on measurements of the position and the mass of all parts that constitute the satellite, via finite element calculation tool estimates. In this paper, we will introduce the gravitational balance requirements and design, and then discuss our predictions for the balance that will be achieved in flight.
publishDate 2016
dc.date.none.fl_str_mv 2016
dc.type.none.fl_str_mv info:eu-repo/semantics/article
format article
dc.identifier.none.fl_str_mv https://hdl.handle.net/20.500.12412/4648
url https://hdl.handle.net/20.500.12412/4648
dc.language.none.fl_str_mv Inglés
language_invalid_str_mv Inglés
dc.relation.none.fl_str_mv The author acknowledges and thanks ASI and CGS for supporting this work.
dc.rights.none.fl_str_mv http://creativecommons.org/licenses/by-nc-nd/4.0/
info:eu-repo/semantics/openAccess
rights_invalid_str_mv http://creativecommons.org/licenses/by-nc-nd/4.0/
eu_rights_str_mv openAccess
dc.source.none.fl_str_mv reponame:Brújula
instname:Universidad Loyola Andalucía
instname_str Universidad Loyola Andalucía
reponame_str Brújula
collection Brújula
repository.name.fl_str_mv
repository.mail.fl_str_mv
_version_ 1869425768546697216
score 15,81155