Carmelo Magnafico, Umberto De Filippis, Francesco Santoli, Carlo Lefevre, Marco Lucente, David Lucchesi, Emiliano Fiorenza, Roberto Peron, Valerio Iafolla
{"title":"Italian Spring Accelerometer measurements of unexpected Non Gravitational Perturbation during BepiColombo second Venus swing-by","authors":"Carmelo Magnafico, Umberto De Filippis, Francesco Santoli, Carlo Lefevre, Marco Lucente, David Lucchesi, Emiliano Fiorenza, Roberto Peron, Valerio Iafolla","doi":"arxiv-2409.02015","DOIUrl":null,"url":null,"abstract":"The Italian Spring Accelerometer (ISA) is a three axis mass-spring\naccelerometer, one of the payloads of the BepiColombo joint space mission\nbetween the European Space Agency (ESA) and the Japan Aerospace Exploration\nAgency (JAXA). At launch in October 2018, BepiColombo started its seven-year\ncruise as a stack of three different modules, overall named Mercury Composite\nSpacecraft (MCS). The spacecraft will provide BepiColombo the necessary Delta V\nto reach Mercury with its electric thrusters and along with one, two and six\ngravity assists, respectively with Earth, Venus and Mercury. The accelerometer\nis accommodated on the Mercury Planetary Orbiter (MPO) module and, jointly with\nthe Ka-band Transponder (KaT) tracking data, will primarily serve the\nBepiColombo Radio Science Experiment (BC-RSE). During the second Venus\nswing-by, strong tidal effect and external perturbations was expected to act on\nthe spacecraft and to become detectable by ISA. The swing-by had a closest\napproach of about 550 km and the gravity gradient expected on the IDA sensing\nelements was perfectly measured. Hence, in this paper, the first direct Gravity\nGradient effect detection generated by an extraterrestrial body is shown.\nNevertheless, around the closest approach, the measurements evidenced a\nspurious acceleration event lasting for several minutes. This work, exploiting\ninformation on the Attitude and Orbit Control System (AOCS) commanded torques,\nfocuses and analyses this ISA acceleration signal, ascribing it to a net force\nreally acting on the MCS spacecraft. Furthermore, using an estimation method,\nthe application point of the force is confined to an area close to the MPO\nradiator.","PeriodicalId":501423,"journal":{"name":"arXiv - PHYS - Space Physics","volume":"109 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - PHYS - Space Physics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.02015","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The Italian Spring Accelerometer (ISA) is a three axis mass-spring
accelerometer, one of the payloads of the BepiColombo joint space mission
between the European Space Agency (ESA) and the Japan Aerospace Exploration
Agency (JAXA). At launch in October 2018, BepiColombo started its seven-year
cruise as a stack of three different modules, overall named Mercury Composite
Spacecraft (MCS). The spacecraft will provide BepiColombo the necessary Delta V
to reach Mercury with its electric thrusters and along with one, two and six
gravity assists, respectively with Earth, Venus and Mercury. The accelerometer
is accommodated on the Mercury Planetary Orbiter (MPO) module and, jointly with
the Ka-band Transponder (KaT) tracking data, will primarily serve the
BepiColombo Radio Science Experiment (BC-RSE). During the second Venus
swing-by, strong tidal effect and external perturbations was expected to act on
the spacecraft and to become detectable by ISA. The swing-by had a closest
approach of about 550 km and the gravity gradient expected on the IDA sensing
elements was perfectly measured. Hence, in this paper, the first direct Gravity
Gradient effect detection generated by an extraterrestrial body is shown.
Nevertheless, around the closest approach, the measurements evidenced a
spurious acceleration event lasting for several minutes. This work, exploiting
information on the Attitude and Orbit Control System (AOCS) commanded torques,
focuses and analyses this ISA acceleration signal, ascribing it to a net force
really acting on the MCS spacecraft. Furthermore, using an estimation method,
the application point of the force is confined to an area close to the MPO
radiator.