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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Hauptverfasser: 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
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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
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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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