The Experts below are selected from a list of 72 Experts worldwide ranked by ideXlab platform

Andrew Gloster - One of the best experts on this subject based on the ideXlab platform.

  • Assembly Integration and Verification Activities for a 2U CubeSat EIRSAT-1
    2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland’s first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme.The Assembly, Integration and Verification (AIV) plan for EIRSAT-1 is central to the philosophy andthedevelopment of the spacecraft. The model philosophy employed for the project is known as the ‘prototype’ approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module(ADM) Platform Element warranta Development Model (DM)in addition to an EQM and a FM, as they have been designed and developed in-house. The engineering qualification model serves asbotha FlatSat for electrical integration testing and as a representative model for testing of software code, patching and operational decisions during the active mission. The EQM is tested to qualification levels and durations during the environmental test campaign. The flight model contains the flight versions of the payloads, ADM Platform Element and the procured hardware Elements. It undergoes acceptance level testing and it is the final spacecraft to be delivered to ESA for flight.After successful completion of the Critical Design Review (CDR) and Ambient Test Readiness Review (ATRR) phases of theproject, the EQM of EIRSAT-1 will beassembled and integrated in University College Dublin. After assembly and integration of the EQM, the project will beginthe ambient test campaign, in which the EQM undergoesambient functional and mission testing. 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
    Proceedings of the 3rd Symposium on Space Educational Activities, 2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland's first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme. The Assembly, Integration and Verification plan for EIRSAT-1 is central to the philosophy and the development of the spacecraft. The model philosophy employed for the project is known as the 'prototype' approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module (ADM) Platform Element warrant a Development Model in addition to an EQM and a FM, as they have been designed and developed in-house. After successful completion of the Critical Design Review and Ambient Test Readiness Review phases 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 ambient test campaign, in which the EQM undergoes ambient functional and mission testing. This work details the preparation and execution of the assembly, integration, and verification activities of EIRSAT-1 EQM.

Ted Saarikko - One of the best experts on this subject based on the ideXlab platform.

  • Platform Provider by Accident
    Business & Information Systems Engineering, 2016
    Co-Authors: Ted Saarikko
    Abstract:

    Recent years have witnessed the rapid emergence of digital technology as not just an enabler, but indeed a material basis for Platform development. However, extant Platform literature does not adequately address strategies related to digital Platforms. Specifically, the notion of Platform coring does not consider how a core is to be identified or the nature of a core in relation to entangled physical and digital materiality. This paper presents a single-case study of a digital Platform for business-to-business services. Results suggest that rather than a specific Platform Element, the core of a digital Platform may be described as a capability to harness the potential of digital technology. Furthermore, Platform coring may be aided by adopting value propositions as a means to conceptualize the process of negotiating mutual benefit among Platform stakeholders. This study contributes to the understanding of digital Platform establishment as it addresses the notion of coring and the emergent process related to the distributed ontology of digital technology and a situated perception of value.

  • Platform Provider by Accident - A Case Study of Digital Platform Coring
    Business & Information Systems Engineering, 2016
    Co-Authors: Ted Saarikko
    Abstract:

    Abstract Recent years have witnessed the rapid emergence of digital technology as not just an enabler, but indeed a material basis for Platform development. However, extant Platform literature does not adequately address strategies related to digital Platforms. Specifically, the notion of Platform coring does not consider how a core is to be identified or the nature of a core in relation to entangled physical and digital materiality. This paper presents a single-case study of a digital Platform for business-to-business services. Results suggest that rather than a specific Platform Element, the core of a digital Platform may be described as a capability to harness the potential of digital technology. Furthermore, Platform coring may be aided by adopting value propositions as a means to conceptualize the process of negotiating mutual benefit among Platform stakeholders. This study contributes to the understanding of digital Platform establishment as it addresses the notion of coring and the emergent process related to the distributed ontology of digital technology and a situated perception of value.

  • A Case Study of Digital Platform Coring
    2016
    Co-Authors: Ted Saarikko
    Abstract:

    Recent years have witnessed the rapid emer- gence of digital technology as not just an enabler, but indeed a material basis for Platform development. How- ever, extant Platform literature does not adequately address strategies related to digital Platforms. Specifically, the notion of Platform coring does not consider how a core is to be identified or the nature of a core in relation to entangled physical and digital materiality. This paper presents a single-case study of a digital Platform for business-to- business services. Results suggest that rather than a specific Platform Element, the core of a digital Platform may be described as a capability to harness the potential of digital technology. Furthermore, Platform coring may be aided by adopting value propositions as a means to conceptualize the process of negotiating mutual benefit among Platform stakeholders. This study contributes to the understanding of digital Platform establishment as it addresses the notion of coring and the emergent process related to the distributed ontology of digital technology and a situated perception of value.

S. Walsh - One of the best experts on this subject based on the ideXlab platform.

  • Assembly Integration and Verification Activities for a 2U CubeSat EIRSAT-1
    2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland’s first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme.The Assembly, Integration and Verification (AIV) plan for EIRSAT-1 is central to the philosophy andthedevelopment of the spacecraft. The model philosophy employed for the project is known as the ‘prototype’ approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module(ADM) Platform Element warranta Development Model (DM)in addition to an EQM and a FM, as they have been designed and developed in-house. The engineering qualification model serves asbotha FlatSat for electrical integration testing and as a representative model for testing of software code, patching and operational decisions during the active mission. The EQM is tested to qualification levels and durations during the environmental test campaign. The flight model contains the flight versions of the payloads, ADM Platform Element and the procured hardware Elements. It undergoes acceptance level testing and it is the final spacecraft to be delivered to ESA for flight.After successful completion of the Critical Design Review (CDR) and Ambient Test Readiness Review (ATRR) phases of theproject, the EQM of EIRSAT-1 will beassembled and integrated in University College Dublin. After assembly and integration of the EQM, the project will beginthe ambient test campaign, in which the EQM undergoesambient functional and mission testing. 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
    Proceedings of the 3rd Symposium on Space Educational Activities, 2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland's first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme. The Assembly, Integration and Verification plan for EIRSAT-1 is central to the philosophy and the development of the spacecraft. The model philosophy employed for the project is known as the 'prototype' approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module (ADM) Platform Element warrant a Development Model in addition to an EQM and a FM, as they have been designed and developed in-house. After successful completion of the Critical Design Review and Ambient Test Readiness Review phases 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 ambient test campaign, in which the EQM undergoes ambient functional and mission testing. This work details the preparation and execution of the assembly, integration, and verification activities of EIRSAT-1 EQM.

Masoud Emam - One of the best experts on this subject based on the ideXlab platform.

  • Assembly Integration and Verification Activities for a 2U CubeSat EIRSAT-1
    2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland’s first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme.The Assembly, Integration and Verification (AIV) plan for EIRSAT-1 is central to the philosophy andthedevelopment of the spacecraft. The model philosophy employed for the project is known as the ‘prototype’ approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module(ADM) Platform Element warranta Development Model (DM)in addition to an EQM and a FM, as they have been designed and developed in-house. The engineering qualification model serves asbotha FlatSat for electrical integration testing and as a representative model for testing of software code, patching and operational decisions during the active mission. The EQM is tested to qualification levels and durations during the environmental test campaign. The flight model contains the flight versions of the payloads, ADM Platform Element and the procured hardware Elements. It undergoes acceptance level testing and it is the final spacecraft to be delivered to ESA for flight.After successful completion of the Critical Design Review (CDR) and Ambient Test Readiness Review (ATRR) phases of theproject, the EQM of EIRSAT-1 will beassembled and integrated in University College Dublin. After assembly and integration of the EQM, the project will beginthe ambient test campaign, in which the EQM undergoesambient functional and mission testing. 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
    Proceedings of the 3rd Symposium on Space Educational Activities, 2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland's first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme. The Assembly, Integration and Verification plan for EIRSAT-1 is central to the philosophy and the development of the spacecraft. The model philosophy employed for the project is known as the 'prototype' approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module (ADM) Platform Element warrant a Development Model in addition to an EQM and a FM, as they have been designed and developed in-house. After successful completion of the Critical Design Review and Ambient Test Readiness Review phases 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 ambient test campaign, in which the EQM undergoes ambient functional and mission testing. This work details the preparation and execution of the assembly, integration, and verification activities of EIRSAT-1 EQM.

Rachel Dunwoody - One of the best experts on this subject based on the ideXlab platform.

  • Assembly Integration and Verification Activities for a 2U CubeSat EIRSAT-1
    2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland’s first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme.The Assembly, Integration and Verification (AIV) plan for EIRSAT-1 is central to the philosophy andthedevelopment of the spacecraft. The model philosophy employed for the project is known as the ‘prototype’ approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module(ADM) Platform Element warranta Development Model (DM)in addition to an EQM and a FM, as they have been designed and developed in-house. The engineering qualification model serves asbotha FlatSat for electrical integration testing and as a representative model for testing of software code, patching and operational decisions during the active mission. The EQM is tested to qualification levels and durations during the environmental test campaign. The flight model contains the flight versions of the payloads, ADM Platform Element and the procured hardware Elements. It undergoes acceptance level testing and it is the final spacecraft to be delivered to ESA for flight.After successful completion of the Critical Design Review (CDR) and Ambient Test Readiness Review (ATRR) phases of theproject, the EQM of EIRSAT-1 will beassembled and integrated in University College Dublin. After assembly and integration of the EQM, the project will beginthe ambient test campaign, in which the EQM undergoesambient functional and mission testing. 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
    Proceedings of the 3rd Symposium on Space Educational Activities, 2020
    Co-Authors: S. Walsh, David Murphy, Maeve Doyle, Joseph Thompson, Rachel Dunwoody, Masoud Emam, Jessica Erkal, Joe Flanagan, Gianluca Fontanesi, Andrew Gloster
    Abstract:

    The Educational Irish Research Satellite, EIRSAT-1, is a project developed by students at University College Dublin that aims to design, build, and launch Ireland's first satellite. EIRSAT-1 is a 2U CubeSat incorporating three novel payloads; GMOD, a gamma-ray detector, EMOD, a thermal coating management experiment, and WBC, a novel attitude control algorithm. The EIRSAT-1 project is carried out with the support of the Education Office of the European Space Agency, under the educational Fly your Satellite! programme. The Assembly, Integration and Verification plan for EIRSAT-1 is central to the philosophy and the development of the spacecraft. The model philosophy employed for the project is known as the 'prototype' approach in which two models of the spacecraft are assembled; an Engineering Qualification Model (EQM) and a Flight Model (FM). The payloads, GMOD and EMOD, and the Antenna Deployment Module (ADM) Platform Element warrant a Development Model in addition to an EQM and a FM, as they have been designed and developed in-house. After successful completion of the Critical Design Review and Ambient Test Readiness Review phases 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 ambient test campaign, in which the EQM undergoes ambient functional and mission testing. This work details the preparation and execution of the assembly, integration, and verification activities of EIRSAT-1 EQM.