With the successful flight of VEGA launcher, a passive laser-ranged satellite for testing general relativity has been put in orbit in 2012. LARES is an Italian Space Agency satellite specifically designed and developed for testing frame dragging, an intriguing prediction of general relativity. The fabric of spacetime is warped by the rotation of a body, e.g. by the Earth’s rotation that drags space and time around it and consequently the orbital plane of a satellite. This last effect is called Lense-Thirring effect and the LARES mission is aimed to measure it with an accuracy of about 1%. The main problem to be solved, in order to reach this objective, is to reduce and to model the classical perturbations, acting on the satellite, at a level well below the Lense-Thirring effect. This has been achieved with the use of a constellation of three laser ranged satellites, a challenging design of the satellite, an optimal choice of the altitude and inclination of the orbit and with the use of the most accurate determinations of the gravitational field of Earth. The paper will describe the mission focusing on the engineering challenges encountered during the development of the program. In particular the extremely high density of the satellite was a concern for the first natural frequency of the satellite and supporting structure that must be higher than 70 Hz.

Engineering challenges of LARES satellite, designed to test the dynamics of general relativity / Paolozzi, Antonio; Ciufolini, Ignazio; Paris, Claudio; Sindoni, Giampiero. - ELETTRONICO. - (2015). (Intervento presentato al convegno International Conference on Structural Engineering Dynamics - ICEDyn 2015 tenutosi a Lagos; Portugal nel 22-24 June 2015).

Engineering challenges of LARES satellite, designed to test the dynamics of general relativity

PAOLOZZI, Antonio;CIUFOLINI, IGNAZIO;PARIS, Claudio;SINDONI, GIAMPIERO
2015

Abstract

With the successful flight of VEGA launcher, a passive laser-ranged satellite for testing general relativity has been put in orbit in 2012. LARES is an Italian Space Agency satellite specifically designed and developed for testing frame dragging, an intriguing prediction of general relativity. The fabric of spacetime is warped by the rotation of a body, e.g. by the Earth’s rotation that drags space and time around it and consequently the orbital plane of a satellite. This last effect is called Lense-Thirring effect and the LARES mission is aimed to measure it with an accuracy of about 1%. The main problem to be solved, in order to reach this objective, is to reduce and to model the classical perturbations, acting on the satellite, at a level well below the Lense-Thirring effect. This has been achieved with the use of a constellation of three laser ranged satellites, a challenging design of the satellite, an optimal choice of the altitude and inclination of the orbit and with the use of the most accurate determinations of the gravitational field of Earth. The paper will describe the mission focusing on the engineering challenges encountered during the development of the program. In particular the extremely high density of the satellite was a concern for the first natural frequency of the satellite and supporting structure that must be higher than 70 Hz.
2015
International Conference on Structural Engineering Dynamics - ICEDyn 2015
aerospace engineering; satellite design; materials; LARES
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Engineering challenges of LARES satellite, designed to test the dynamics of general relativity / Paolozzi, Antonio; Ciufolini, Ignazio; Paris, Claudio; Sindoni, Giampiero. - ELETTRONICO. - (2015). (Intervento presentato al convegno International Conference on Structural Engineering Dynamics - ICEDyn 2015 tenutosi a Lagos; Portugal nel 22-24 June 2015).
File allegati a questo prodotto
File Dimensione Formato  
Paolozzi_Engineering_2015.pdf

solo gestori archivio

Tipologia: Documento in Post-print (versione successiva alla peer review e accettata per la pubblicazione)
Licenza: Tutti i diritti riservati (All rights reserved)
Dimensione 630.61 kB
Formato Adobe PDF
630.61 kB Adobe PDF   Contatta l'autore

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/786806
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus ND
  • ???jsp.display-item.citation.isi??? ND
social impact