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Author: Zachary Scott Decker
Publisher:
ISBN:
Category :
Languages : en
Pages : 101
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Book Description
This research conducts a broad systems-based analysis of CubeSat engineering, with a focus on testing, failures, and their relationship to program cost, in order to assess multiple build approaches with a goal of maintaining the advantages of CubeSat missions while increasing reliability. In this work, the multiple approaches are called “beta build strategies,” and we show that satellite engineering groups with minimal experience can increase their probability of success by building two flight-model versions of their satellite, allowing for more exhaustive and potentially failure-inducing testing to be conducted on the first (beta version) satellite. This differentiates itself from the standard CubeSat build approach, which is typically to build a flat sat, then an engineering model, and then a flight model of the satellite. Frequently with CubeSat development, the additional expense of building a flight-like engineering model is avoided. However, in this work we consider the probability of success and overall cost impact for multiple approaches toward the flight build. We find that by spending an additional 33% of the planned program cost, a team which plans to take this alternate approach from the beginning can build and launch two flight-model versions of their spacecraft, increasing probability of success by 30%. This cost corresponds to a 40% saving from the scenario in which the decision to build a second flight-model spacecraft is made only after the first fails. The question which this analysis tries to answer is not, “how does a group spend the least amount of money to get their first CubeSat into space?” but rather, “how does a group spend the least amount of money to get a CubeSat into space that works?”
Author: Zachary Scott Decker
Publisher:
ISBN:
Category :
Languages : en
Pages : 101
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Book Description
This research conducts a broad systems-based analysis of CubeSat engineering, with a focus on testing, failures, and their relationship to program cost, in order to assess multiple build approaches with a goal of maintaining the advantages of CubeSat missions while increasing reliability. In this work, the multiple approaches are called “beta build strategies,” and we show that satellite engineering groups with minimal experience can increase their probability of success by building two flight-model versions of their satellite, allowing for more exhaustive and potentially failure-inducing testing to be conducted on the first (beta version) satellite. This differentiates itself from the standard CubeSat build approach, which is typically to build a flat sat, then an engineering model, and then a flight model of the satellite. Frequently with CubeSat development, the additional expense of building a flight-like engineering model is avoided. However, in this work we consider the probability of success and overall cost impact for multiple approaches toward the flight build. We find that by spending an additional 33% of the planned program cost, a team which plans to take this alternate approach from the beginning can build and launch two flight-model versions of their spacecraft, increasing probability of success by 30%. This cost corresponds to a 40% saving from the scenario in which the decision to build a second flight-model spacecraft is made only after the first fails. The question which this analysis tries to answer is not, “how does a group spend the least amount of money to get their first CubeSat into space?” but rather, “how does a group spend the least amount of money to get a CubeSat into space that works?”
Author: Kyle B. Hurst
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
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Book Description
The nanosatellite industry is expanding rapidly, as academic and private institutions develop new technologies for experimentation on orbit. These "CubeSats" are resource constrained, complex socio-technical systems that have complicated interdependencies across multiple domains. To improve understanding and reduce ambiguity, systems engineers apply a variety of modeling frameworks to model system behavior. Introduced in 2007, the Engineering Systems Multiple- Domain Matrix (ES-MDM) framework addresses the interdependencies of a complex engineering system, such as a CubeSat, across five domains: environmental, social, functional, technical and process. Using the Free-space Lasercom and Radiation Experiment (FLARE) CubeSat constellation as an example engineering system case, the ES-MDM is constructed using the qualitative knowledge construction framework to model and analyze the system drivers, stakeholders, objectives, function, objects and processes of the system. The primary objective of this analysis is to provide a structured systems design approach for nanosatellite development that encompasses the entire system holistically. The second objective is to analyze the interactions and interdependencies within a highly-constrained system and determine key design nodes that are critical to system flexibility. The third objective is to evaluate the ability of the ES-MDM methodology to analyze a highly-constrained system. The fourth objective of thesis is to provide recommendations for future work to improve the ESMDM framework and the s7102 Massachusetts Institute of Technology. Integrated Design and Management Program.
Author: Hubert Anton Moser
Publisher: Springer
ISBN: 3319038958
Category : Technology & Engineering
Languages : en
Pages : 342
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Book Description
This book focuses on systems engineering, systems thinking, and how that thinking can be learned in practice. It describes a novel analytical framework based on activity theory for understanding how systems thinking evolves and how it can be improved to support multidisciplinary teamwork in the context of system development and systems engineering. This method, developed using data collected over four years from three different small space systems engineering organizations, can be applied in a wide variety of work activities in the context of engineering design and beyond in order to monitor and analyze multidisciplinary interactions in working teams over time. In addition, the book presents a practical strategy called WAVES (Work Activity for a Evolution of Systems engineering and thinking), which fosters the practical learning of systems thinking with the aim of improving process development in different industries. The book offers an excellent resource for researchers and practitioners interested in systems thinking and in solutions to support its evolution. Beyond its contribution to a better understanding of systems engineering, systems thinking and how it can be learned in real-world contexts, it also introduce a suitable analysis framework that helps to bridge the gap between the latest social science research and engineering research.
Author: National Academies of Sciences, Engineering, and Medicine
Publisher: National Academies Press
ISBN: 030944263X
Category : Science
Languages : en
Pages : 131
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Book Description
Space-based observations have transformed our understanding of Earth, its environment, the solar system and the universe at large. During past decades, driven by increasingly advanced science questions, space observatories have become more sophisticated and more complex, with costs often growing to billions of dollars. Although these kinds of ever-more-sophisticated missions will continue into the future, small satellites, ranging in mass between 500 kg to 0.1 kg, are gaining momentum as an additional means to address targeted science questions in a rapid, and possibly more affordable, manner. Within the category of small satellites, CubeSats have emerged as a space-platform defined in terms of (10 cm x 10 cm x 10 cm)- sized cubic units of approximately 1.3 kg each called "U's." Historically, CubeSats were developed as training projects to expose students to the challenges of real-world engineering practices and system design. Yet, their use has rapidly spread within academia, industry, and government agencies both nationally and internationally. In particular, CubeSats have caught the attention of parts of the U.S. space science community, which sees this platform, despite its inherent constraints, as a way to affordably access space and perform unique measurements of scientific value. The first science results from such CubeSats have only recently become available; however, questions remain regarding the scientific potential and technological promise of CubeSats in the future. Achieving Science with CubeSats reviews the current state of the scientific potential and technological promise of CubeSats. This report focuses on the platform's promise to obtain high- priority science data, as defined in recent decadal surveys in astronomy and astrophysics, Earth science and applications from space, planetary science, and solar and space physics (heliophysics); the science priorities identified in the 2014 NASA Science Plan; and the potential for CubeSats to advance biology and microgravity research. It provides a list of sample science goals for CubeSats, many of which address targeted science, often in coordination with other spacecraft, or use "sacrificial," or high-risk, orbits that lead to the demise of the satellite after critical data have been collected. Other goals relate to the use of CubeSats as constellations or swarms deploying tens to hundreds of CubeSats that function as one distributed array of measurements.
Author: Azad M. Madni
Publisher: Springer
ISBN: 331962217X
Category : Technology & Engineering
Languages : en
Pages : 1169
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Book Description
The theme of this volume on systems engineering research is disciplinary convergence: bringing together concepts, thinking, approaches, and technologies from diverse disciplines to solve complex problems. Papers presented at the Conference on Systems Engineering Research (CSER), March 23-25, 2017 at Redondo Beach, CA, are included in this volume. This collection provides researchers in academia, industry, and government forward-looking research from across the globe, written by renowned academic, industry and government researchers.
Author: Juan Cepeda-Rizo
Publisher: CRC Press
ISBN: 1000511081
Category : Technology & Engineering
Languages : en
Pages : 278
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Book Description
Have you ever wondered how NASA designs, builds, and tests spacecrafts and hardware for space? How is it that wildly successful programs such as the Mars Exploration Rovers could produce a rover that lasted over ten times the expected prime mission duration? Or build a spacecraft designed to visit two orbiting destinations and last over 10 years when the fuel ran out? This book was written by NASA/JPL engineers with experience across multiple projects, including the Mars rovers, Mars helicopter, and Dawn ion propulsion spacecraft in addition to many more missions and technology demonstration programs. It provides useful and practical approaches to solving the most complex thermal-structural problems ever attempted for design spacecraft to survive the severe cold of deep space, as well as the unforgiving temperature swings on the surface of Mars. This is done without losing sight of the fundamental and classical theories of thermodynamics and structural mechanics that paved the way to more pragmatic and applied methods such finite element analysis and Monte Carlo ray tracing, for example. Features: Includes case studies from NASA’s Jet Propulsion Laboratory, which prides itself in robotic exploration of the solar system, as well as flyting the first cubeSAT to Mars. Enables spacecraft designer engineers to create a design that is structurally and thermally sound, and reliable, in the quickest time afforded. Examines innovative low-cost thermal and power systems. Explains how to design to survive rocket launch, the surfaces of Mars and Venus. Suitable for practicing professionals as well as upper-level students in the areas of aerospace, mechanical, thermal, electrical, and systems engineering, Thermal and Structural Electronic Packaging Analysis for Space and Extreme Environments provides cutting-edge information on how to design, and analyze, and test in the fast-paced and low-cost small satellite environment and learn techniques to reduce the design and test cycles without compromising reliability. It serves both as a reference and a training manual for designing satellites to withstand the structural and thermal challenges of extreme environments in outer space.
Author: Sharanabasaweshwara Ashok Asundi
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
ABSTRACT : CubeSats have been recognized globally for their potential utility for revolutionizing the space industry. However, with the exception of the CubeSat specification, the development approach to date has been mostly ad hoc. Based on lessons learned from the design and development of a terrestrial ground robot, a systematic approach utilizing systems engineering techniques has been developed for CubeSats. The approach uses a top-down design methodology to translate mission definitions into basic building blocks that then facilitate a bottom-up development and fabrication process. The limitations imposed by the CubeSats size, weight, and power on the design process are addressed in the developed approach. To describe the traceability from mission requirements to subsystem component selection, design, and integration, SwampSat, a University of Florida CubeSat, is used as an example. Within this context of traceability, several unique design features of CubeSats are identified and described. These include (i) novel multifunctional structural elements, (ii) distributed processing to reduce power consumption yet provide complex computational capability, and (iii) efficient computational algorithm amenable to low power device implementations. To demonstrate features (ii) and (iii), Murrells version of the extended Kalman filter is adapted for SwampSats attitude determination subsystem and demonstrated for three sensor configurations. The considered sensor configurations were based on (a) sun sensor and magnetometer combination, (b) magnetometer and synthesized magnetic rate combination, and (c) magnetometer only. All three sensor configuration utilized spacecraft angular rate information for attitude propagation. Simulations involving detailed sensor characteristics were performed to evaluate the performance of the three sensor configurations and it was demonstrated that configuration (c) was best in terms of overall error but worst in terms of convergence.
Author: Azad M. Madni
Publisher: Springer Nature
ISBN: 3030820831
Category : Technology & Engineering
Languages : en
Pages : 709
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Book Description
This volume comprises papers from the 18th Conference on Systems Engineering Research (CSER). The theme of this volume, “Recent Trends and Advances in Model-Based Systems Engineering,” reflects the fact that systems engineering is undergoing a transformation motivated by mission and system complexity and enabled by technological advances such as model-based systems engineering, digital engineering, and the convergence of systems engineering with other disciplines. This conference is focused on exploring recent trends and advances in model-based systems engineering (MBSE) and the synergy of MBSE with simulation technology and digital engineering. Contributors have submitted papers on MBSE methods, modeling approaches, integration of digital engineering with MBSE, standards, modeling languages, ontologies and metamodels, and economics analysis of MBSE to respond to the challenges posed by 21st century systems. What distinguishes this volume are the latest advances in MBSE research, the convergence of MBSE with digital engineering, and recent advances in applied research in MBSE, including growing convergence with systems science and decision science. This volume is appropriate as a reference text in graduate engineering courses in Model-Based Systems Engineering.
Author: Chantal Cappelletti
Publisher: Academic Press
ISBN: 012817885X
Category : Technology & Engineering
Languages : en
Pages : 500
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Book Description
CubeSat Handbook: From Mission Design to Operations is the first book solely devoted to the design, manufacturing, and in-orbit operations of CubeSats. Beginning with an historical overview from CubeSat co-inventors Robert Twiggs and Jordi Puig-Suari, the book is divided into 6 parts with contributions from international experts in the area of small satellites and CubeSats. It covers topics such as standard interfaces, on-board & ground software, industry standards in terms of control algorithms and sub-systems, systems engineering, standards for AITV (assembly, integration, testing and validation) activities, and launch regulations. This comprehensive resource provides all the information needed for engineers and developers in industry and academia to successfully design and launch a CubeSat mission. - Provides an overview on all aspects that a CubeSat developer needs to analyze during mission design and its realization - Features practical examples on how to design and deal with possible issues during a CubeSat mission - Covers new developments and technologies, including ThinSats and PocketQubeSats
Author: Francesco Branz
Publisher: Elsevier
ISBN: 0128245425
Category : Technology & Engineering
Languages : en
Pages : 838
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Book Description
Next Generation of CubeSats and SmallSats: Enabling Technologies, Missions, and Markets provides a comprehensive understanding of the small and medium sized satellite approach and its potentialities and limitations. The book analyzes promising applications (e.g., constellations and distributed systems, small science platforms that overachieve relative to their development time and cost) as paradigm-shifting solutions for space exploitation, with an analysis of market statistics and trends and a prediction of where the technologies, and consequently, the field is heading in the next decade. The book also provides a thorough analysis of CubeSat potentialities and applications, and addresses unique technical approaches and systems strategies. Throughout key sections (introduction and background, technology details, systems, applications, and future prospects), the book provides basic design tools scaled to the small satellite problem, assesses the technological state-of-the-art, and describes the most recent advancements with a look to the near future. This new book is for aerospace engineering professionals, advanced students, and designers seeking a broad view of the CubeSat world with a brief historical background, strategies, applications, mission scenarios, new challenges and upcoming advances. - Presents a comprehensive and systematic view of the technologies and space missions related to nanosats and smallsats - Discusses next generation technologies, up-coming advancements and future perspectives - Features the most relevant CubeSat launch initiatives from NASA, ESA, and from developing countries, along with an overview of the New Space CubeSat market
