Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations

This thesis presents an exploratory analysis of the electromagnetic environment faced by spacecrafts during commercial launches to Low Earth Orbit (LEO), considering both radiated emission levels and electromagnetic compatibility (EMC) requirements as described in various launch providers’ Payload U...

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Autores:: Barrios García, Adriana Marcela

Tipo de recurso:: Trabajo de grado de pregrado

Fecha de publicación:: 2025

Institución:: Universidad de Antioquia

Repositorio:: Repositorio UdeA

Idioma:: eng

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network_acronym_str	UDEA2
network_name_str	Repositorio UdeA
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dc.title.eng.fl_str_mv	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
title	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
spellingShingle	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations Electromagnetic compatibility Compatibilidad electromagnética Launch vehicles (Astronautics) Vehículos de lanzamiento (Astronáutica) Correlation (Statistics) Correlación (Estadística) Electromagnetic interference - Detection Interferencia electromagnética - Detección Payloads (Aerospace engineering) Cargas útiles (Ingeniería aeroespacial) Astronautics - Systems engineering Astronáutica - Ingeniería de sistemas Standardization Normalización http://id.loc.gov/authorities/subjects/sh85042167 http://id.loc.gov/authorities/subjects/sh85075056 http://id.loc.gov/authorities/subjects/sh85033032 http://id.loc.gov/authorities/subjects/sh2015001199 http://id.loc.gov/authorities/subjects/sh2005004552 http://id.loc.gov/authorities/subjects/sh85008963 http://id.loc.gov/authorities/subjects/sh85127309 ODS 9: Industria, innovación e infraestructura. Construir infraestructuras resilientes, promover la industrialización inclusiva y sostenible y fomentar la innovación
title_short	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
title_full	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
title_fullStr	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
title_full_unstemmed	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
title_sort	Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations
dc.creator.fl_str_mv	Barrios García, Adriana Marcela
dc.contributor.advisor.none.fl_str_mv	Puerta Ibarra, Juan Francisco
dc.contributor.author.none.fl_str_mv	Barrios García, Adriana Marcela
dc.subject.lcsh.none.fl_str_mv	Electromagnetic compatibility Compatibilidad electromagnética Launch vehicles (Astronautics) Vehículos de lanzamiento (Astronáutica) Correlation (Statistics) Correlación (Estadística) Electromagnetic interference - Detection Interferencia electromagnética - Detección Payloads (Aerospace engineering) Cargas útiles (Ingeniería aeroespacial) Astronautics - Systems engineering Astronáutica - Ingeniería de sistemas Standardization Normalización
topic	Electromagnetic compatibility Compatibilidad electromagnética Launch vehicles (Astronautics) Vehículos de lanzamiento (Astronáutica) Correlation (Statistics) Correlación (Estadística) Electromagnetic interference - Detection Interferencia electromagnética - Detección Payloads (Aerospace engineering) Cargas útiles (Ingeniería aeroespacial) Astronautics - Systems engineering Astronáutica - Ingeniería de sistemas Standardization Normalización http://id.loc.gov/authorities/subjects/sh85042167 http://id.loc.gov/authorities/subjects/sh85075056 http://id.loc.gov/authorities/subjects/sh85033032 http://id.loc.gov/authorities/subjects/sh2015001199 http://id.loc.gov/authorities/subjects/sh2005004552 http://id.loc.gov/authorities/subjects/sh85008963 http://id.loc.gov/authorities/subjects/sh85127309 ODS 9: Industria, innovación e infraestructura. Construir infraestructuras resilientes, promover la industrialización inclusiva y sostenible y fomentar la innovación
dc.subject.lcshuri.none.fl_str_mv	http://id.loc.gov/authorities/subjects/sh85042167 http://id.loc.gov/authorities/subjects/sh85075056 http://id.loc.gov/authorities/subjects/sh85033032 http://id.loc.gov/authorities/subjects/sh2015001199 http://id.loc.gov/authorities/subjects/sh2005004552 http://id.loc.gov/authorities/subjects/sh85008963 http://id.loc.gov/authorities/subjects/sh85127309
dc.subject.ods.none.fl_str_mv	ODS 9: Industria, innovación e infraestructura. Construir infraestructuras resilientes, promover la industrialización inclusiva y sostenible y fomentar la innovación
description	This thesis presents an exploratory analysis of the electromagnetic environment faced by spacecrafts during commercial launches to Low Earth Orbit (LEO), considering both radiated emission levels and electromagnetic compatibility (EMC) requirements as described in various launch providers’ Payload User’s Guides (PUGs). Correlation analyses and cluster-based segmentation were applied to identify which structural and operational variables influence emissions and constraints. Globally, the type of propulsion system (ρ = –0.81) and rocket L/D dimensions ratio (ρ = –0.46) were found to correlate with launch vehicle emissions, while payload constraints were mainly influenced by the mission type (ρ = –0.55) and payload capacity (ρ = –0.33). In specific clusters, other variables such as vehicle mass (ρ = 0.81), number of stages (ρ = –0.81), and fairing L/D ratio (ρ = 0.94) also showed associations with frequency range or electric field intensity. Regarding launch sites, it was found that LC-36 tends to generate higher emissions relative the launch vehicle itself and in some cases, these emissions also exceed the maximum allowed for the spacecrafts. Although no quantitative relationship was found between environmental conditions and launch frequency, most launch sites are located in Köppen CFA and CSB climates, due more to logistical and infrastructure factors than environmental suitability. In terms of EMC requirements, 52 entries were identified across 11 categories. Most are general guidelines or non-binding recommendations, with limited normative references and test criteria, highlighting the urgent need for clearer standardization—particularly for the validation of fully integrated systems.
publishDate	2025
dc.date.accessioned.none.fl_str_mv	2025-11-13T12:57:01Z
dc.date.issued.none.fl_str_mv	2025
dc.type.none.fl_str_mv	Trabajo de grado - Pregrado
dc.type.coar.none.fl_str_mv	http://purl.org/coar/resource_type/c_7a1f
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dc.type.content.none.fl_str_mv	Text
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dc.type.driver.none.fl_str_mv	info:eu-repo/semantics/bachelorThesis
dc.type.version.none.fl_str_mv	info:eu-repo/semantics/draft
format	http://purl.org/coar/resource_type/c_7a1f
status_str	draft
dc.identifier.citation.none.fl_str_mv	Barrios García, A. M. “Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations ”, Bachelor’s degree project, Aerospace Engineering, Universidad de Antioquia, Carmen de Viboral, Antioquia, Colombia, 2025.
dc.identifier.uri.none.fl_str_mv	https://hdl.handle.net/10495/48217
identifier_str_mv	Barrios García, A. M. “Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations ”, Bachelor’s degree project, Aerospace Engineering, Universidad de Antioquia, Carmen de Viboral, Antioquia, Colombia, 2025.
url	https://hdl.handle.net/10495/48217
dc.language.iso.none.fl_str_mv	eng
language	eng
dc.relation.references.none.fl_str_mv	[1] T. Discussion, “What is EMC? Electromagnetic Compatibility = EMI (Interference) + EMS (Susceptibility) Explained!” 2022. [Online]. Available: https://www.youtube.com/watch?v=uQrHUvpfpk&t [2] D. Duchesne, “What is the difference between EMC and EMI?” 2024. [Online]. Available: https://www.nemko.com/blog/emc-vs-emi-whats-the-difference [3] Tektronix, “How to prepare for successful EMI and EMC testing,” 2025. [Online]. Available: https://www.tek.com/en/solutions/application/emi-emc-testing [4] E. Lidman, “Electromagnetic Compatibility Testing of Cubesats,” Ph.D. dissertation, Lulea Univ. of Technology, 2024. [5] G. G. S. F. Center, “General Environmental Verification Standard (GEVS) for GSFC Flight Programs and Projects,” Goddard Space Flight Center, Tech. Rep., Apr. 2021. [Online]. Available: http://standards.gsfc.nasa.gov [6] J. Radtke, E. Stoll, H. Lewis, and B. B. Virgili, “The Impact Of The Increase In Small Satellite Launch Traffic On The Long-Term Evolution Of The Space Debris Environment,” in 7th European Conference on Space Debris, ESA Space Debris Office, 2017. [Online]. Available: https://conference.sdo.esoc.esa.int/proceedings/sdc7/paper/353 [7] B. Tran, “Satellite Launch Market Growth: How Many Satellites Are Being Launched?” 2025. [Online]. Available: https://patentpc.com/blog/satellite-launch-market-growth-how-many-satellites-are-being-launched [8] M. Swartwout and C. O. December, “Number of small satellite launches continues to grow, with no end in sight,” Aerospace America, 2025. [Online]. Available: https://aerospaceamerica.aiaa.org/year-in-review/number-of-small-satellite-launches-continues-to-grow-with-no-end-in-sight/ [9] S. E. T. Corp., “Rideshare Payload User’s Guide,” Space Exploration Technologies Corp., Tech. Rep., Sep. 2024. [10] N. Aeronautics and S. A. (NASA), “NASA-HDBK-4002 Mitigating In-Space Charging Effects – A Guideline Measurement System Identification,” NASA, Tech. Rep., Oct. 2017. [Online]. Available: http://standards.nasa.gov [11] E. C. for Space Standardization (ECSS), “ECSS-E-ST-20-07C-Rev.2,” European Cooperation for Space Standardization (ECSS), Tech. Rep., 1 2022. [12] D. of Defense Interface Standard, “Requirements For The Control Of Electromagnetic Interference Characteristics Of Subsystems And Equipment,” Department of Defense Interface Standard, Tech. Rep., 12 2015. [Online]. Available: http://www.everyspec.com [13] E. Tran, “Environment/EMC/EMI,” Carnegie Mellon University, Tech. Rep., 1999. [Online]. Available: http://www.emclab.umr.edu [14] Time and Date, “Time and Date,” 2025. [Online]. Available: https://www.timeanddate.com/weather [15] W. Spark, “Weather Spark,” 2025. [Online]. Available: https://es.weatherspark.com [16] G. Space, “Gunter’s Space Page - Information on spaceflight, launch vehicles and satellites,” 2025. [Online]. Available: https://space.skyrocket.de [17] E. Kyle, “Space Launch Report,” Space Launch Report, Tech. Rep., 5 2025. [Online]. Available: https://launchreport.neocities.org [18] O. W. in Data, “Annual number of objects launched into space.” University of Oxford & Global Change Data Lab, Tech. Rep., 2025. [Online]. Available: https://ourworldindata.org/grapher/yearly-number-of-objects-launched-into-outer-space?time=latest [19] N. Air and S. Museum, “All About Rockets,” 2025. [Online]. Available: https://airandspace.si.edu/learn/programs/soar-together/rockets-2 [20] G. R. Center, “Payload Systems,” 2025. [Online]. Available: https://www1.grc.nasa.gov/beginners-guide-to-aeronautics/payload-systems/ [21] J. M. Logsdon, “Launch bases,” 4 2023. [Online]. Available: https://www.britannica.com/technology/launch-vehicle/Launch-bases [22] A. Medvedev, A. K. Nedaivoda, M. F. Jensen, and E. F. Laursen, “Angara Launch System Mission Planner’s Guide,” International Launch Services, Tech. Rep., 12 2002. [Online]. Available: http://www.ilslaunch.com/missionplanner [23] I. L. Services, “Proton Launch System Mission Planner’s Guide,” International Launch Services, Tech. Rep., 7 2009. [Online]. Available: www.ilslaunch.comwww.ilslaunch.com [24] N. Grumman, “Minotaur IV-VI User Guide,” Northrop Grumman, Tech. Rep., 9 2020. [25] A. Cen, Z. Gao, and R. S. Lei, “LM-3A Series Launch Vehicle User’s Manual,” China Aerospace Science And Technology Corporation (CASC), Tech. Rep., 2011. [26] M. L. Services, “- User’s Manual,” Mitsubishi Launch Services, Tech. Rep., 2 2015. [Online]. Available: http://h2a.mhi.co.jp/en/index.html [27] R. Lab, “Electron Payload User’s Guide,” Rocket Lab, Tech. Rep., 11 2022. [28] SpaceX, “Falcon User’s Guide,” SpaceX, Tech. Rep., 9 2021. [29] Arianespace, “Ariane 6 User’s Manual for Multi-Launch Service,” Arianespace, Tech. Rep., 7 2021. [Online]. Available: www.arianespace.com [30] B. Origin, “New Glenn Payload User’s Guide,” Blue Origin, Tech. Rep., 10 2018. [31] A. space, “ROCKET 4 - Payload User’s Guide,” Astra space, Tech. Rep., 11 2022. [32] Arianespace, “Soyuz User’s Manual Issue 2,” Arianespace, Tech. Rep., 5 2018. [Online]. Available: www.arianespace.com [33] Wikipedia, “Correlacion,” 2025. [Online]. Available: https://es.wikipedia.org/wiki/Correlacion [34] G. for Geeks, “Random Forest Algorithm in Machine Learning,” 2025. [Online]. Available: https://www.geeksforgeeks.org/random-forest-algorithm-in-machine-learning/ [35] IBM, “What Is Random Forest,” IBM, Tech. Rep., 2025. [Online]. Available: https://www.ibm.com/think/topics/random-forest [36] D. B. Camp, “What is the Variance Inflation Factor (VIF),” 2024. [37] T. I. TEAM, “Variance Inflation Factor (VIF),” 5 2025. [Online]. Available: https://www.investopedia.com/terms/v/variance-inflation-factor.asp [38] B. M. Benito, “Everything You Don’t Need to Know About Variance Inflation Factors,” Tech. Rep., 2023. [39] J. Dick, “Guide to Writing Requirements,” INCOSE, Tech. Rep., 7 2023. [Online]. Available: http://www.incose.org
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dc.publisher.place.none.fl_str_mv	El Carmen de Viboral, Colombia
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publisher.none.fl_str_mv	Universidad de Antioquia
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spelling	Puerta Ibarra, Juan FranciscoBarrios García, Adriana Marcela2025-11-13T12:57:01Z2025Barrios García, A. M. “Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations ”, Bachelor’s degree project, Aerospace Engineering, Universidad de Antioquia, Carmen de Viboral, Antioquia, Colombia, 2025.https://hdl.handle.net/10495/48217This thesis presents an exploratory analysis of the electromagnetic environment faced by spacecrafts during commercial launches to Low Earth Orbit (LEO), considering both radiated emission levels and electromagnetic compatibility (EMC) requirements as described in various launch providers’ Payload User’s Guides (PUGs). Correlation analyses and cluster-based segmentation were applied to identify which structural and operational variables influence emissions and constraints. Globally, the type of propulsion system (ρ = –0.81) and rocket L/D dimensions ratio (ρ = –0.46) were found to correlate with launch vehicle emissions, while payload constraints were mainly influenced by the mission type (ρ = –0.55) and payload capacity (ρ = –0.33). In specific clusters, other variables such as vehicle mass (ρ = 0.81), number of stages (ρ = –0.81), and fairing L/D ratio (ρ = 0.94) also showed associations with frequency range or electric field intensity. Regarding launch sites, it was found that LC-36 tends to generate higher emissions relative the launch vehicle itself and in some cases, these emissions also exceed the maximum allowed for the spacecrafts. Although no quantitative relationship was found between environmental conditions and launch frequency, most launch sites are located in Köppen CFA and CSB climates, due more to logistical and infrastructure factors than environmental suitability. In terms of EMC requirements, 52 entries were identified across 11 categories. Most are general guidelines or non-binding recommendations, with limited normative references and test criteria, highlighting the urgent need for clearer standardization—particularly for the validation of fully integrated systems.Esta tesis realiza un análisis exploratorio del entorno electromagnético que enfrentan las cargas útiles en lanzamientos comerciales a órbita baja terrestre (LEO), considerando tanto los niveles de emisión radiada como los requisitos de compatibilidad electromagnética (EMC) descritos en los Payload User’s Guides (PUGs) de distintos lanzadores. Se aplicaron correlaciones y segmentaciones por clúster para identificar qué variables estructurales y operacionales influyen en las emisiones y restricciones. A nivel general, se observó que el tipo de propulsión (ρ = –0,81) y la relación L/D del cohete (ρ = –0,46) se correlacionan con las emisiones generadas por el lanzador, mientras que el tipo de misión (ρ = –0,55) y la capacidad de carga útil (ρ = –0,33) influyen sobre las restricciones impuestas a la carga útil. En clústeres específicos, otras variables como la masa (ρ = 0,81), el número de etapas (ρ = –0,81) y la relación L/D del carenado (ρ = 0,94) también mostraron asociación con el rango de frecuencia o campo eléctrico permitido. Respecto al entorno del sitio de lanzamiento, se identificó que LC-36 tiende a generar emisiones más altas relativas al vehículo de lanzamiento, y que en algunos casos estas superan también las restricciones impuestas a la carga útil. Aunque no se encontró una relación cuantitativa entre condiciones ambientales y frecuencia de lanzamientos, se evidenció una alta concentración en climas tipo CFA y CSB, lo que responde más a decisiones logísticas e infraestructura disponible. En cuanto a los requisitos, se identificaron 52 en total, distribuidos en 11 categorías. La mayoría corresponde a lineamientos generales o sugerencias sin criterios de prueba definidos, y con baja presencia de referencias normativas, lo que pone de manifiesto la necesidad de mayor estandarización, especialmente para validar sistemas integrados.RESUMEN ........................................................................... 12 ABSTRACT ......................................................................... 13 I INTRODUCTION ............................................................... 14 II PROBLEM STATEMENT .................................................. 17 III JUSTIFICATION ................................................................ 19 IV OBJECTIVES .................................................................... 20 A General Objective ................................................................ 20 B Specific Objectives ................................................................. 20 V SCOPE ............................................................................. 21 VI LITERATURE REVIEW .................................................. 22 A Electromagnetic Compatibility (EMC) ......................... 22 1 Types of EMC Phenomena ........................................... 23 2 Sources of EMI ................................................................... 24 B Electromagnetic Compatibility in Space Launches ....... 25 1 Involved actors ................................................................. 25 2 EMC interactions between launch actors ................... 26 3 EMC in the mission design process ......................... 27 C Applicable EMC Standards and Technical Regulations ... 28 1 Regulatory Standard ........................................................ 28 2 Technical Standards ...................................................... 29 3 Tailoring ............................................................................ 30 4 Handbook .......................................................................... 30 5 Payload User’s Guide (PUG) ................................. 31 VII METHODOLOGY ............................................................. 32 A Part I: Statistical Analysis of the Electromagnetic Environment .......... 33 1 Structure and parameters of the database ................ 34 2 Analysis of the electromagnetic environment by actor type ........ 36 3 Launch Vehicle maximum radiated emissions under worst-case scenario .... 41 4 Spacecraft maximum radiated emissions ..................... 46 5 Comparison of launch site emissions with launch vehicle and spacecraft limits .... 47 a Launch site radiated emissions relative to spacecraft limits ............ 47 b Launch site radiated emissions relative to launch vehicle emissions ..... 49 6 Environmental factors influence on launches ............ 50 7 Pattern analysis and justification for emission data segmentation ...... 55 8 Explanation of the analysis sequence and methodology flow ........ 56 9 Clustering Method and determination of the optimal number of clusters ..... 57 10 Cluster analysis process ................................................ 58 11 Comparison with the general model ............................ 59 B Part II: Analysis of Electromagnetic Compatibility (EMC) Requirements ...... 60 1 EMC normative review context in the PUGs ............... 60 2 Comparative Review of EMC-Related Requirements Across PUGs .... 61 VIII RESULTS ..................................................................... 63 A General Analysis of the Electromagnetic Environment ............. 63 1 Launch vehicle maximum radiated emissions ............ 63 2 Spacecraft Maximum Radiated Emissions ................... 67 3 Launch site radiated emissions relative to spacecraft limits ........ 71 4 Launch site radiated emissions relative to launch vehicle emissions ........ 72 5 Influence of environmental conditions on launch activity .......... 73 B Cluster-Based Segmentation ................................................ 82 1 Cluster 0 – Light and slim launch vehicles with low electromagnetic emissions ...... 85 2 Cluster 1 – Heavy launch vehicle with highest electromagnetic emissions ...... 96 3 Cluster 2 – Robust launch vehicles with moderate electromagnetic emissions ...... 98 C Analysis of Requirements and Referenced Standards in the PUGs ...... 107 1 Comparative Requirement Analysis across PUGs ........ 107 2 Referenced, Suggested, or Absent Standards in the PUGs ...... 111 IX CONCLUSIONS ................................................................. 115 X RECOMMENDATIONS AND FUTURE WORK .................... 117 REFERENCES .................................................................... 119 APPENDIX ......................................................................... 123 APPENDIX A. Abstract accepted for presentation at the 76th IAC .......... 123PregradoIngeniero Aeroespacial123 páginasapplication/pdfengUniversidad de AntioquiaIngeniería AeroespacialEl Carmen de Viboral, ColombiaFacultad de IngenieríaCampus El Carmen de Viboralhttp://creativecommons.org/licenses/by-sa/4.0/info:eu-repo/semantics/openAccessAttribution-ShareAlike 4.0 Internationalhttp://purl.org/coar/access_right/c_abf2Electromagnetic compatibilityCompatibilidad electromagnéticaLaunch vehicles (Astronautics)Vehículos de lanzamiento (Astronáutica)Correlation (Statistics)Correlación (Estadística)Electromagnetic interference - DetectionInterferencia electromagnética - DetecciónPayloads (Aerospace engineering)Cargas útiles (Ingeniería aeroespacial)Astronautics - Systems engineeringAstronáutica - Ingeniería de sistemasStandardizationNormalizaciónhttp://id.loc.gov/authorities/subjects/sh85042167http://id.loc.gov/authorities/subjects/sh85075056http://id.loc.gov/authorities/subjects/sh85033032http://id.loc.gov/authorities/subjects/sh2015001199http://id.loc.gov/authorities/subjects/sh2005004552http://id.loc.gov/authorities/subjects/sh85008963http://id.loc.gov/authorities/subjects/sh85127309ODS 9: Industria, innovación e infraestructura. Construir infraestructuras resilientes, promover la industrialización inclusiva y sostenible y fomentar la innovaciónElectromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical CorrelationsTrabajo de grado - Pregradohttp://purl.org/coar/resource_type/c_7a1fhttp://purl.org/redcol/resource_type/TPTexthttp://purl.org/coar/version/c_b1a7d7d4d402bcceinfo:eu-repo/semantics/bachelorThesisinfo:eu-repo/semantics/draft[1] T. Discussion, “What is EMC? Electromagnetic Compatibility = EMI (Interference) + EMS (Susceptibility) Explained!” 2022. [Online]. Available: https://www.youtube.com/watch?v=uQrHUvpfpk&t[2] D. Duchesne, “What is the difference between EMC and EMI?” 2024. [Online]. Available: https://www.nemko.com/blog/emc-vs-emi-whats-the-difference[3] Tektronix, “How to prepare for successful EMI and EMC testing,” 2025. [Online]. Available: https://www.tek.com/en/solutions/application/emi-emc-testing[4] E. Lidman, “Electromagnetic Compatibility Testing of Cubesats,” Ph.D. dissertation, Lulea Univ. of Technology, 2024.[5] G. G. S. F. Center, “General Environmental Verification Standard (GEVS) for GSFC Flight Programs and Projects,” Goddard Space Flight Center, Tech. Rep., Apr. 2021. [Online]. Available: http://standards.gsfc.nasa.gov[6] J. Radtke, E. Stoll, H. Lewis, and B. B. Virgili, “The Impact Of The Increase In Small Satellite Launch Traffic On The Long-Term Evolution Of The Space Debris Environment,” in 7th European Conference on Space Debris, ESA Space Debris Office, 2017. [Online]. Available: https://conference.sdo.esoc.esa.int/proceedings/sdc7/paper/353[7] B. Tran, “Satellite Launch Market Growth: How Many Satellites Are Being Launched?” 2025. [Online]. Available: https://patentpc.com/blog/satellite-launch-market-growth-how-many-satellites-are-being-launched[8] M. Swartwout and C. O. December, “Number of small satellite launches continues to grow, with no end in sight,” Aerospace America, 2025. [Online]. Available: https://aerospaceamerica.aiaa.org/year-in-review/number-of-small-satellite-launches-continues-to-grow-with-no-end-in-sight/[9] S. E. T. Corp., “Rideshare Payload User’s Guide,” Space Exploration Technologies Corp., Tech. Rep., Sep. 2024.[10] N. Aeronautics and S. A. (NASA), “NASA-HDBK-4002 Mitigating In-Space Charging Effects – A Guideline Measurement System Identification,” NASA, Tech. Rep., Oct. 2017. [Online]. Available: http://standards.nasa.gov[11] E. C. for Space Standardization (ECSS), “ECSS-E-ST-20-07C-Rev.2,” European Cooperation for Space Standardization (ECSS), Tech. Rep., 1 2022.[12] D. of Defense Interface Standard, “Requirements For The Control Of Electromagnetic Interference Characteristics Of Subsystems And Equipment,” Department of Defense Interface Standard, Tech. Rep., 12 2015. [Online]. Available: http://www.everyspec.com[13] E. 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

Electromagnetic Compatibility in Spacecraft Launches. Analysis and Interpretation of the Phenomenon Using Statistical Correlations

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