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The Educational Irish Research Satellite, EIRSAT-1, is a project developed bystudents at University College Dublin that aims to design, build, and launchIreland's first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novelpayloads; GMOD, a gamma-ray detector, EMOD, a thermal coating managementexperiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 projectis carried out with the support of the Education Office of the European SpaceAgency, under the educational Fly your Satellite! programme. The Assembly,Integration and Verification plan for EIRSAT-1 is central to the philosophy andthe development of the spacecraft. The model philosophy employed for theproject is known as the 'prototype' approach in which two models of thespacecraft are assembled; an Engineering Qualification Model (EQM) and a FlightModel (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module(ADM) platform element warrant a Development Model in addition to an EQM and aFM, as they have been designed and developed in-house. After successfulcompletion of the Critical Design Review and Ambient Test Readiness Reviewphases of the project, the EQM of EIRSAT-1 will be assembled and integrated.After assembly and integration of the EQM, the project will begin the ambienttest campaign, in which the EQM undergoes ambient functional and missiontesting. This work details the preparation and execution of the assembly,integration, and verification activities of EIRSAT-1 EQM.

Assembly, Integration, and Verification Activities for a 2U CubeSat, EIRSAT-1