Lares Mission: Engineering Aspects
Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Paolozzi, A. [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2015 |
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| Anmerkung: |
© AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 |
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| Übergeordnetes Werk: |
Enthalten in: Aerotecnica missili & spazio - [Cham] : Springer International Publishing, 2001, 94(2015), 1 vom: 01. Jan., Seite 23-30 |
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| Übergeordnetes Werk: |
volume:94 ; year:2015 ; number:1 ; day:01 ; month:01 ; pages:23-30 |
| Links: |
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| DOI / URN: |
10.1007/BF03404685 |
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| Katalog-ID: |
SPR038612739 |
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| 520 | |a Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. | ||
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| 700 | 1 | |a Gabrielli, A. |4 aut | |
| 700 | 1 | |a Paris, C. |4 aut | |
| 700 | 1 | |a Sindoni, G. |4 aut | |
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10.1007/BF03404685 doi (DE-627)SPR038612739 (SPR)BF03404685-e DE-627 ger DE-627 rakwb eng Paolozzi, A. verfasserin aut Lares Mission: Engineering Aspects 2015 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. Ciufolini, I. aut Gabrielli, A. aut Paris, C. aut Sindoni, G. aut Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 94(2015), 1 vom: 01. Jan., Seite 23-30 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:94 year:2015 number:1 day:01 month:01 pages:23-30 https://dx.doi.org/10.1007/BF03404685 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 94 2015 1 01 01 23-30 |
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10.1007/BF03404685 doi (DE-627)SPR038612739 (SPR)BF03404685-e DE-627 ger DE-627 rakwb eng Paolozzi, A. verfasserin aut Lares Mission: Engineering Aspects 2015 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. Ciufolini, I. aut Gabrielli, A. aut Paris, C. aut Sindoni, G. aut Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 94(2015), 1 vom: 01. Jan., Seite 23-30 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:94 year:2015 number:1 day:01 month:01 pages:23-30 https://dx.doi.org/10.1007/BF03404685 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 94 2015 1 01 01 23-30 |
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10.1007/BF03404685 doi (DE-627)SPR038612739 (SPR)BF03404685-e DE-627 ger DE-627 rakwb eng Paolozzi, A. verfasserin aut Lares Mission: Engineering Aspects 2015 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. Ciufolini, I. aut Gabrielli, A. aut Paris, C. aut Sindoni, G. aut Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 94(2015), 1 vom: 01. Jan., Seite 23-30 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:94 year:2015 number:1 day:01 month:01 pages:23-30 https://dx.doi.org/10.1007/BF03404685 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 94 2015 1 01 01 23-30 |
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10.1007/BF03404685 doi (DE-627)SPR038612739 (SPR)BF03404685-e DE-627 ger DE-627 rakwb eng Paolozzi, A. verfasserin aut Lares Mission: Engineering Aspects 2015 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. Ciufolini, I. aut Gabrielli, A. aut Paris, C. aut Sindoni, G. aut Enthalten in Aerotecnica missili & spazio [Cham] : Springer International Publishing, 2001 94(2015), 1 vom: 01. Jan., Seite 23-30 (DE-627)1047764040 (DE-600)2960384-5 2524-6968 nnns volume:94 year:2015 number:1 day:01 month:01 pages:23-30 https://dx.doi.org/10.1007/BF03404685 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 94 2015 1 01 01 23-30 |
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Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 |
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Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 |
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Abstract LARES is a satellite of the Italian Space Agency, successfully launched with the new VEGA launcher in the occasion of its inaugural flight, VV01. It was put in a circular orbit at 1450 km altitude. This altitude was required to reduce atmospheric drag, whereas the satellite was designed to minimize the non-gravitational perturbations acting on the surface of the satellite. This was of paramount importance because the mission objective is to test Einstein general relativity, and any unmodeled effect could spoil the accuracy of the relativistic measurement. With the optimal design achieved, this non-gravitational unmodeled effects are maintained below 1% of frame-dragging or Lense-Thirring effect. This effect is the orbital node shift induced by the Earth rotation as predicted by general relativity. To achieve the accuracy required for the test, it was conceived a constellation of three laser ranged satellites (LAGEOS 1, LAGEOS 2 and LARES) along with the latest determination of the Earth gravitational field by GRACE satellite. The satellite is a passive system and embedded with 92 Cube Corner Reflectors that have the properties of reflecting back to the emitting ground station the laser pulses, thus allowing its precise orbital determination. In this paper engineering aspects of the mission will be addressed. © AIDAA Associazione Italiana di Aeronautica e Astronautica 2015 |
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