SpIRIT Mission: In-Orbit Results and Technology Demonstrations
The Space Industry Responsive Intelligent Thermal (SpIRIT) 6U CubeSat is a mission led by The University of Melbourne in cooperation with the Italian Space Agency. Launched in a 510 km Polar Sun Synchronous Orbit in December 2023, SpIRIT carries multiple subsystems for scientific and technology demo...
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creator | Trenti, Michele del Castillo, Miguel Ortiz Mearns, Robert McRobbie, Jack Therakam, Clint Chapman, Airlie Woods, Andrew Morgan, Jonathan Barraclough, Simon Mallo, Ivan Rodriguez Baroni, Giulia Fiore, Fabrizio Evangelista, Yuri Campana, Riccardo Guzman, Alejandro Hedderman, Paul |
description | The Space Industry Responsive Intelligent Thermal (SpIRIT) 6U CubeSat is a
mission led by The University of Melbourne in cooperation with the Italian
Space Agency. Launched in a 510 km Polar Sun Synchronous Orbit in December
2023, SpIRIT carries multiple subsystems for scientific and technology
demonstration. The main payload is the HERMES instrument for detection of
high-energy astrophysics transients (Gamma Ray Bursts), and for studies of
their variability at scales below 1 ms. The satellite includes a novel thermal
management system for its class, based on a Stirling-cycle cooler and
deployable thermal radiator, designed to cool HERMES to reduce instrumental
background noise. A low-latency communication subsystem based on a sat-phone
network is supporting rapid transmission of time-critical data and
telecommands. SpIRIT is also equipped with a set of RGB and thermal IR cameras,
connected to an on-board image processing unit with artificial intelligence
capabilities for autonomous feature recognition. To effectively manage all
interfaces between different subsystems and mission stakeholders, the
University of Melbourne developed an instrument control unit (PMS) which
operates all payloads. PMS also provides backup uninterruptible power to the
HERMES instrument through a supercapacitor-based UPS for safe instrument
shutdown in case of platform power interruptions. This paper first presents a
mission and payload overview, and early in-orbit results, along with lessons
learned throughout the mission. This work not only sheds light on the novelty
of some of the on-board technologies onboard and on their potential impact to
enable greater utilization of CubeSats for scientific missions, but also offers
insights into the practical challenges and accomplishments related to
developing and operating a multi-organization CubeSat with a complex array of
instruments and systems. |
doi_str_mv | 10.48550/arxiv.2407.14034 |
format | Article |
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mission led by The University of Melbourne in cooperation with the Italian
Space Agency. Launched in a 510 km Polar Sun Synchronous Orbit in December
2023, SpIRIT carries multiple subsystems for scientific and technology
demonstration. The main payload is the HERMES instrument for detection of
high-energy astrophysics transients (Gamma Ray Bursts), and for studies of
their variability at scales below 1 ms. The satellite includes a novel thermal
management system for its class, based on a Stirling-cycle cooler and
deployable thermal radiator, designed to cool HERMES to reduce instrumental
background noise. A low-latency communication subsystem based on a sat-phone
network is supporting rapid transmission of time-critical data and
telecommands. SpIRIT is also equipped with a set of RGB and thermal IR cameras,
connected to an on-board image processing unit with artificial intelligence
capabilities for autonomous feature recognition. To effectively manage all
interfaces between different subsystems and mission stakeholders, the
University of Melbourne developed an instrument control unit (PMS) which
operates all payloads. PMS also provides backup uninterruptible power to the
HERMES instrument through a supercapacitor-based UPS for safe instrument
shutdown in case of platform power interruptions. This paper first presents a
mission and payload overview, and early in-orbit results, along with lessons
learned throughout the mission. This work not only sheds light on the novelty
of some of the on-board technologies onboard and on their potential impact to
enable greater utilization of CubeSats for scientific missions, but also offers
insights into the practical challenges and accomplishments related to
developing and operating a multi-organization CubeSat with a complex array of
instruments and systems.</description><identifier>DOI: 10.48550/arxiv.2407.14034</identifier><language>eng</language><subject>Physics - High Energy Astrophysical Phenomena ; Physics - Instrumentation and Methods for Astrophysics</subject><creationdate>2024-07</creationdate><rights>http://arxiv.org/licenses/nonexclusive-distrib/1.0</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>228,230,780,885</link.rule.ids><linktorsrc>$$Uhttps://arxiv.org/abs/2407.14034$$EView_record_in_Cornell_University$$FView_record_in_$$GCornell_University$$Hfree_for_read</linktorsrc><backlink>$$Uhttps://doi.org/10.48550/arXiv.2407.14034$$DView paper in arXiv$$Hfree_for_read</backlink></links><search><creatorcontrib>Trenti, Michele</creatorcontrib><creatorcontrib>del Castillo, Miguel Ortiz</creatorcontrib><creatorcontrib>Mearns, Robert</creatorcontrib><creatorcontrib>McRobbie, Jack</creatorcontrib><creatorcontrib>Therakam, Clint</creatorcontrib><creatorcontrib>Chapman, Airlie</creatorcontrib><creatorcontrib>Woods, Andrew</creatorcontrib><creatorcontrib>Morgan, Jonathan</creatorcontrib><creatorcontrib>Barraclough, Simon</creatorcontrib><creatorcontrib>Mallo, Ivan Rodriguez</creatorcontrib><creatorcontrib>Baroni, Giulia</creatorcontrib><creatorcontrib>Fiore, Fabrizio</creatorcontrib><creatorcontrib>Evangelista, Yuri</creatorcontrib><creatorcontrib>Campana, Riccardo</creatorcontrib><creatorcontrib>Guzman, Alejandro</creatorcontrib><creatorcontrib>Hedderman, Paul</creatorcontrib><title>SpIRIT Mission: In-Orbit Results and Technology Demonstrations</title><description>The Space Industry Responsive Intelligent Thermal (SpIRIT) 6U CubeSat is a
mission led by The University of Melbourne in cooperation with the Italian
Space Agency. Launched in a 510 km Polar Sun Synchronous Orbit in December
2023, SpIRIT carries multiple subsystems for scientific and technology
demonstration. The main payload is the HERMES instrument for detection of
high-energy astrophysics transients (Gamma Ray Bursts), and for studies of
their variability at scales below 1 ms. The satellite includes a novel thermal
management system for its class, based on a Stirling-cycle cooler and
deployable thermal radiator, designed to cool HERMES to reduce instrumental
background noise. A low-latency communication subsystem based on a sat-phone
network is supporting rapid transmission of time-critical data and
telecommands. SpIRIT is also equipped with a set of RGB and thermal IR cameras,
connected to an on-board image processing unit with artificial intelligence
capabilities for autonomous feature recognition. To effectively manage all
interfaces between different subsystems and mission stakeholders, the
University of Melbourne developed an instrument control unit (PMS) which
operates all payloads. PMS also provides backup uninterruptible power to the
HERMES instrument through a supercapacitor-based UPS for safe instrument
shutdown in case of platform power interruptions. This paper first presents a
mission and payload overview, and early in-orbit results, along with lessons
learned throughout the mission. This work not only sheds light on the novelty
of some of the on-board technologies onboard and on their potential impact to
enable greater utilization of CubeSats for scientific missions, but also offers
insights into the practical challenges and accomplishments related to
developing and operating a multi-organization CubeSat with a complex array of
instruments and systems.</description><subject>Physics - High Energy Astrophysical Phenomena</subject><subject>Physics - Instrumentation and Methods for Astrophysics</subject><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>GOX</sourceid><recordid>eNpjYJA0NNAzsTA1NdBPLKrILNMzMjEw1zM0MTA24WSwCy7wDPIMUfDNLC7OzM-zUvDM0_UvSsosUQhKLS7NKSlWSMxLUQhJTc7Iy8_JT69UcEnNzc8rLilKLAEqL-ZhYE1LzClO5YXS3Azybq4hzh66YJviC4oycxOLKuNBNsaDbTQmrAIAMRY1kw</recordid><startdate>20240719</startdate><enddate>20240719</enddate><creator>Trenti, Michele</creator><creator>del Castillo, Miguel Ortiz</creator><creator>Mearns, Robert</creator><creator>McRobbie, Jack</creator><creator>Therakam, Clint</creator><creator>Chapman, Airlie</creator><creator>Woods, Andrew</creator><creator>Morgan, Jonathan</creator><creator>Barraclough, Simon</creator><creator>Mallo, Ivan Rodriguez</creator><creator>Baroni, Giulia</creator><creator>Fiore, Fabrizio</creator><creator>Evangelista, Yuri</creator><creator>Campana, Riccardo</creator><creator>Guzman, Alejandro</creator><creator>Hedderman, Paul</creator><scope>GOX</scope></search><sort><creationdate>20240719</creationdate><title>SpIRIT Mission: In-Orbit Results and Technology Demonstrations</title><author>Trenti, Michele ; del Castillo, Miguel Ortiz ; Mearns, Robert ; McRobbie, Jack ; Therakam, Clint ; Chapman, Airlie ; Woods, Andrew ; Morgan, Jonathan ; Barraclough, Simon ; Mallo, Ivan Rodriguez ; Baroni, Giulia ; Fiore, Fabrizio ; Evangelista, Yuri ; Campana, Riccardo ; Guzman, Alejandro ; Hedderman, Paul</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-arxiv_primary_2407_140343</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Physics - High Energy Astrophysical Phenomena</topic><topic>Physics - Instrumentation and Methods for Astrophysics</topic><toplevel>online_resources</toplevel><creatorcontrib>Trenti, Michele</creatorcontrib><creatorcontrib>del Castillo, Miguel Ortiz</creatorcontrib><creatorcontrib>Mearns, Robert</creatorcontrib><creatorcontrib>McRobbie, Jack</creatorcontrib><creatorcontrib>Therakam, Clint</creatorcontrib><creatorcontrib>Chapman, Airlie</creatorcontrib><creatorcontrib>Woods, Andrew</creatorcontrib><creatorcontrib>Morgan, Jonathan</creatorcontrib><creatorcontrib>Barraclough, Simon</creatorcontrib><creatorcontrib>Mallo, Ivan Rodriguez</creatorcontrib><creatorcontrib>Baroni, Giulia</creatorcontrib><creatorcontrib>Fiore, Fabrizio</creatorcontrib><creatorcontrib>Evangelista, Yuri</creatorcontrib><creatorcontrib>Campana, Riccardo</creatorcontrib><creatorcontrib>Guzman, Alejandro</creatorcontrib><creatorcontrib>Hedderman, Paul</creatorcontrib><collection>arXiv.org</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Trenti, Michele</au><au>del Castillo, Miguel Ortiz</au><au>Mearns, Robert</au><au>McRobbie, Jack</au><au>Therakam, Clint</au><au>Chapman, Airlie</au><au>Woods, Andrew</au><au>Morgan, Jonathan</au><au>Barraclough, Simon</au><au>Mallo, Ivan Rodriguez</au><au>Baroni, Giulia</au><au>Fiore, Fabrizio</au><au>Evangelista, Yuri</au><au>Campana, Riccardo</au><au>Guzman, Alejandro</au><au>Hedderman, Paul</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>SpIRIT Mission: In-Orbit Results and Technology Demonstrations</atitle><date>2024-07-19</date><risdate>2024</risdate><abstract>The Space Industry Responsive Intelligent Thermal (SpIRIT) 6U CubeSat is a
mission led by The University of Melbourne in cooperation with the Italian
Space Agency. Launched in a 510 km Polar Sun Synchronous Orbit in December
2023, SpIRIT carries multiple subsystems for scientific and technology
demonstration. The main payload is the HERMES instrument for detection of
high-energy astrophysics transients (Gamma Ray Bursts), and for studies of
their variability at scales below 1 ms. The satellite includes a novel thermal
management system for its class, based on a Stirling-cycle cooler and
deployable thermal radiator, designed to cool HERMES to reduce instrumental
background noise. A low-latency communication subsystem based on a sat-phone
network is supporting rapid transmission of time-critical data and
telecommands. SpIRIT is also equipped with a set of RGB and thermal IR cameras,
connected to an on-board image processing unit with artificial intelligence
capabilities for autonomous feature recognition. To effectively manage all
interfaces between different subsystems and mission stakeholders, the
University of Melbourne developed an instrument control unit (PMS) which
operates all payloads. PMS also provides backup uninterruptible power to the
HERMES instrument through a supercapacitor-based UPS for safe instrument
shutdown in case of platform power interruptions. This paper first presents a
mission and payload overview, and early in-orbit results, along with lessons
learned throughout the mission. This work not only sheds light on the novelty
of some of the on-board technologies onboard and on their potential impact to
enable greater utilization of CubeSats for scientific missions, but also offers
insights into the practical challenges and accomplishments related to
developing and operating a multi-organization CubeSat with a complex array of
instruments and systems.</abstract><doi>10.48550/arxiv.2407.14034</doi><oa>free_for_read</oa></addata></record> |
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subjects | Physics - High Energy Astrophysical Phenomena Physics - Instrumentation and Methods for Astrophysics |
title | SpIRIT Mission: In-Orbit Results and Technology Demonstrations |
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