Gotowe bibliografie tematyczne / CubeSat

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Gotowa bibliografia na temat „CubeSat”

Autor: Grafiati

Data publikacji: 4 czerwca 2021

Data aktualizacji: 25 lipca 2025

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Artykuły w czasopismach na temat "CubeSat"

De Leon, Michael B., Ulysses B. Ante, Madelene S. Velasco, et al. "3D-Printing for Cube Satellites (CubeSats): Philippines‘ Perspectives." Engineering Innovations 1 (March 25, 2022): 13–27. http://dx.doi.org/10.4028/p-35niy3.

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The increase in space exploration missions in recent years gave way to the development of a volume-efficient and cost-effective nanosatellite like the cube satellite (CubeSat) which can be developed and fabricated in a relatively short time. With its size and design, CubeSat parts like casings can be produced and assembled through 3D printing to produce inexpensive satellites. Research in this area is undeniably important to maximize the rapid development of CubeSats. While progress has been made, challenges remain in applying 3D printing technology in the development of CubeSats. In this pape

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Xu, Duo, Honghao Yue, Yong Zhao, et al. "Improved A* Algorithm for Path Planning Based on CubeSats In-Orbit Electromagnetic Transfer System." Aerospace 11, no. 5 (2024): 394. http://dx.doi.org/10.3390/aerospace11050394.

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For future large-scale CubeSat applications in orbit, the deployer must accommodate a greater number of CubeSats and facilitate cluster releases. This paper introduces an improved A* algorithm tailored for CubeSat in-orbit transfer path planning. Unlike the traditional A* algorithm, this enhanced version incorporates a path coordination strategy to manage congestion caused by the simultaneous transfer of many CubeSats, ensuring they reach their designated release positions smoothly and thus significantly boosting the efficiency of CubeSat transfers. Additionally, the algorithm develops a cost

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Şanlı, Alper, Tuncay Yunus Erkeç, Melih Beceren, and Mehmet Furkan Kemallı. "Architecture of Stratosphere Rocket for Cubesats." Volume 04 Issue 01 vm04, is01 (2023): 14–22. http://dx.doi.org/10.23890/ijast.vm04is01.0102.

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Cubesat missions are evolving, and because of their high efficiency, they are becoming more common. Cubesats can go to space more easily because of their compact size. Launch vehicles provide great opportunity for us to reach space and high altitudes of the atmosphere. Today, cubesats are launched to high altitudes for experimental purposes with the help of launch vehicles. In this investigation, a novel launch vehicle was created to match the cubesat's specifications. A stable launch vehicle that can take a cubesat the size of 3U to the stratospheric layer has undergone its first design and e

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Menchinelli, Alessandro, Francesca Ingiosi, Ludovico Pamphili, et al. "A Reliability Engineering Approach for Managing Risks in CubeSats." Aerospace 5, no. 4 (2018): 121. http://dx.doi.org/10.3390/aerospace5040121.

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Besides large-scale space missions, the spread of CubeSats for a variety of applications is increasingly requiring the development of systematic approaches for risk management. Being these applications are based on components with low TRL (Technology Readiness Level) or with limited performance data, it is required to define approaches which ensure a systematic perspective. This paper aims to present a reliability engineering approach based on FMECA (Failure Mode, Effects, and Criticality Analysis) to manage CubeSat reliability data and prioritize criticalities early in the design phase. The a

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Sibanda, Matthew, and Robert Ryk van Zyl. "Practical electromagnetic compatibility studies of a CubeSat." Journal of Engineering, Design and Technology 14, no. 4 (2016): 770–80. http://dx.doi.org/10.1108/jedt-04-2014-0025.

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Purpose Incorporating electromagnetic compatibility (EMC) in the design life of traditional satellites is entrenched in the satellite industry. However, EMC treatment of CubeSats has not been widely pursued, for various possible reasons. CubeSats are a young technology platform initially intended for students and researchers at universities to create awareness and excitement amongst them for space technology. This and other factors limited the need for stringent EMC planning. As CubeSats mature in complexity, the success of future missions will rely on incorporating proper EMC designs in their

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Alanazi, Abdulaziz, and Jeremy Straub. "Engineering Methodology for Student-Driven CubeSats." Aerospace 6, no. 5 (2019): 54. http://dx.doi.org/10.3390/aerospace6050054.

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CubeSats are widely used by universities and research institutions all over the world. Their popularity is generally attributed to the use of low-cost components, free student labor and simple design. They have been shown to encourage Science, Technology, Engineering and Math (STEM) students to become involved in designing, implementing and testing a real functioning spacecraft system. Projects like this encourage students from different disciplines to team up to design and build CubeSats, providing interdisciplinary work experience. Participating students vary in their expertise in developing

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Lu, Sining, Panagiotis Ioannis Theoharis, Raad Raad, et al. "A Survey on CubeSat Missions and Their Antenna Designs." Electronics 11, no. 13 (2022): 2021. http://dx.doi.org/10.3390/electronics11132021.

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CubeSats are a class of miniaturized satellites that have become increasingly popular in academia and among hobbyists due to their short development time and low fabrication cost. Their compact size, lightweight characteristics, and ability to form a swarm enables them to communicate directly with one another to inspire new ideas on space exploration, space-based measurements, and implementation of the latest technology. CubeSat missions require specific antenna designs in order to achieve optimal performance and ensure mission success. Over the past two decades, a plethora of antenna designs

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O O, Afolabi, Adediji A. T, Ewetumo T, and Adedayo K. D. "A Survey of Locally Available Subsystems for Cubesat Projects in Nigerian Market." IOSR Journal of Applied Physics 16, no. 6 (2024): 22–26. https://doi.org/10.9790/4861-1606012226.

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There are quite a lot of cube sat subsystems that can be procured on the African continent to develop Cube Satellite (CubeSats). However these are not noticed by many relevant professionals that can design and integrate them to functional CubeSats in Nigeria.frican countries And other This is despite the ever increasing role this class of satellite is playing in educational, scientific research and commercial satellite weather, earth observation and communication services. The paper also identified basic physics principles and mathematical models for the prediction of the attitude of a spacecr

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Villela, Thyrso, Cesar A. Costa, Alessandra M. Brandão, Fernando T. Bueno, and Rodrigo Leonardi. "Towards the Thousandth CubeSat: A Statistical Overview." International Journal of Aerospace Engineering 2019 (January 10, 2019): 1–13. http://dx.doi.org/10.1155/2019/5063145.

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CubeSats have become an interesting innovation in the space sector. Such platforms are being used for several space applications, such as education, Earth remote sensing, science, and defense. As of May 31st, 2018, 855 CubeSats had been launched. Remote sensing application is the main sector in which CubeSats are being used, corresponding to about 45% of all applications. This fact indicates the commercial potential of such a platform. Fifty eight countries have already been involved with developing CubeSats. The most used CubeSat configuration is 3U (about 64%), followed by 1U (18%), while 6U

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Sri, Ram Deepak Akella, and Srinivas Baswanth Pappula Sashendra. "Advancements in CubeSat development: Applications and structural analysis." i-manager's Journal on Structural Engineering 13, no. 2 (2024): 13. https://doi.org/10.26634/jste.13.2.21618.

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This paper explores the development, applications, and structural analysis of CubeSats, small standardized satellites that have revolutionized space missions through their affordability and versatility. Initiated by professors Jordi Puig-Suari and Bob Twiggs in 1999, CubeSats were designed for educational and research purposes, enabling the testing of space technologies in low Earth orbit (LEO). Initially dominated by academic institutions, CubeSat launches saw significant growth from commercial and amateur sectors by 2014. CubeSats have expanded from LEO operations to interplanetary missions,

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Rozprawy doktorskie na temat "CubeSat"

Erlank, Alexander Olaf. "Development of CubeStar : a CubeSat-compatible star tracker." Thesis, Stellenbosch : Stellenbosch University, 2013. http://hdl.handle.net/10019.1/85746.

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Thesis (MEng)-- Stellenbosch University, 2013.<br>ENGLISH ABSTRACT: The next generation of CubeSats will require accurate attitude knowledge throughout orbit for advanced science payloads and high gain antennas. A star tracker can provide the required performance, but star trackers have traditionally been too large, expensive and power hungry to be included on a CubeSat. The aim of this project is to develop and demonstrate a CubeSat compatible star tracker. Subsystems from two other CubeSat components, CubeSense and CubeComputer, were combined with a sensitive, commercial image sensor a

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Slettebo, Christian. "CubeSub : A CUBESAT BASED SUBMERSIBLE TESTBED FOR SPACE TECHNOLOGY." Thesis, KTH, Flygdynamik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-198521.

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This report is a Master’s Thesis in Aerospace Engineering, performed at the NASA Ames Research Center. It describes the development of the CubeSub, a submersible testbed compatible with the CubeSat form factor. The CubeSub will be used to mature technology and operational procedures to be used in space exploration, and possibly also as a tool for exploration of Earthly environments. CubeSats are carried as payloads, either containing technology to be tested or experiments and sensors for scientific use. The CubeSub is designed to be built up by modules, which can be assembled in different conf

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castello, brian. "CUBESAT MISSION PLANNING TOOLBOX." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/787.

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We are in an era of massive spending cuts in educational institutions, aerospace companies and governmental entities. Educational institutions are pursuing more training for less money, aerospace companies are reducing the cost of gaining ight heritage and the government is cutting budgets and their response times. Organizations are accomplishing this improved efficiency by moving away from large-scale satellite projects and developing pico and nanosatellites following the CubeSat specifications. One of the major challenges of developing satellites to the standard CubeSat mission requirements

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Tapparel, Pierre-André. "CDMS pour cubesat /." Sion, 2006. http://doc.rero.ch/search.py?recid=8376&ln=fr.

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Horký, Jan. "Řídicí jednotka pro CubeSat." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2017. http://www.nusl.cz/ntk/nusl-318165.

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Cílem práce je návrh univerzální řídicí jednotky pro CubeSat založené na obvodu FPGA. Taková jednotka doposud nebyla komerčně dostupná a navržená jednotka má tak dobrý potenciál zaplnit příslušné místo na trhu komponent pro CubeSat. Celá jednotka je navržena z komerčně dostupných komponent. Návrh jednotky je proveden tak, aby umožnil její funkci ve vesmírném prostředí. Stav konfigurace FPGA je pravidelně kontrolován a v případě zjištěné chyby dochází automaticky k rekonfiguraci FPGA a návratu jednotky do výchozího stavu. Jednotka obsahuje sadu senzorů, které monitorují její stav a v případě po

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Harris, Anthony D. "NPS CubeSat Launcher-lite sequence." Thesis, Monterey, Calif. : Naval Postgraduate School, 2009. http://edocs.nps.edu/npspubs/scholarly/theses/2009/Jun/09Jun%5FHarris.pdf.

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Thesis (M.S. in Space Systems Operations)--Naval Postgraduate School, June 2009.<br>Thesis Advisor(s): Newman, James H. "June 2009." Description based on title screen as viewed on July 10, 2009. Author(s) subject terms: NPSCuL, NPSCuL-Lite, P-POD, Sequencer, Launcher, Launch Vehicle, Microcontroller, Space, Satellite. Includes bibliographical references (p. 167-168). Also available in print.

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Hicks, Christina M. "NPS CubeSat Launcher program management." Thesis, Monterey, California : Naval Postgraduate School, 2009. http://edocs.nps.edu/npspubs/scholarly/theses/2009/Sep/09Sep%5FHicks.pdf.

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Thesis (M.S. in Space Systems Operations)--Naval Postgraduate School, September 2009.<br>Thesis Advisor(s): Newman, James H. "September 2009." Description based on title screen as viewed on November 10, 2009. Author(s) subject terms: NPSCuL, CubeSat, Launcher, P-POD, ABC, Aft Bulkhead Carrier, Centaur, ESPA, Secondary Payload, Program Management. Includes bibliographical references (p. 61-63). Also available in print.

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Zohar, Guy G. "AD-HOC REGIONAL COVERAGE CONSTELLATIONS OF CUBESATS USING SECONDARY LAUNCHES." DigitalCommons@CalPoly, 2013. https://digitalcommons.calpoly.edu/theses/927.

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As development of CubeSat based architectures increase, methods of deploying constellations of CubeSats are required to increase functionality of future systems. Given their low cost and quickly increasing launch opportunities, large numbers of CubeSats can easily be developed and deployed in orbit. However, as secondary payloads, CubeSats are severely limited in their options for deployment into appropriate constellation geometries. This thesis examines the current methods for deploying cubes and proposes new and efficient geometries using secondary launch opportunities. Due to the current de

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Frances, Matas Jordi. "Internal Wireless Bus for a CubeSat." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for elektronikk og telekommunikasjon, 2013. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-23088.

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NTNU (Norwegian University of Science and Technology) hosts NUTS (NTNU Test Satellite), which is mainly envisioned as an educational satellite where most tasks are performed by students while supported by university staff. As a peculiarity this CubeSat, unlike many others, is not based on the PC104 Standard. It is, instead, developed around a backplane approach, similar to a motherboard on a desktop computer. This novel approach left us without the possibility to use readily available commercial modules for CubeSats and also with the responsibility to design an ad-hoc solution for power distri

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Griffith, Robert C. "Mobile Cubesat Command and Control (MC3)." Thesis, Monterey, California. Naval Postgraduate School, 2011. http://hdl.handle.net/10945/5591.

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Approved for public release; distribution is unlimited.<br>The Mobile CubeSat Command and Control (MC3) program will become the ground segment of the Colony II satellite program. The MC3 ground station contains Commercial Off-the-Shelf (COTS) hardware with Government Off-the-Shelf (GOTS) software making it an affordable option for government agencies and universities participating in the Colony II program. Further, the MC3 program provides educational opportunities to students and training to space professionals in satellite communications. This thesis analyzes the MC3 program from the program

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Książki na temat "CubeSat"

Italy) IAA Conference on University Satellite Missions and CubeSat Workshop (5th 2020 Rome. Fifth IAA Conference on University Satellite Missions and CubeSat Workshop 2020: Proceedings of the 5th Conference on Unbiversity Satellite Missions and CubeSat Workshop, held January 28-31, 2020, Rome, Italy. Published for the American Astronautical Society by Univelt, 2020.

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Kwon, Young W. Direct manufacturing of CubeSat using 3-D digital printer and determination of its mechanical properties. Naval Postgraduate School, 2010.

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Italy) IAA Conference on University Satellite Missions and CubeSat Workshop (4th 2017 Rome. Fourth IAA Conference on University Satellite Missions and CubeSat Workshop 2017: Proceedings of the 4th International Academy of Astronautics Conference on University Satellite Missions and CubeSat Workshop, held December 4-7, 2017, Rome, Italy. Edited by Graziani Filippo editor, International Academy of Astronautics, and American Astronautical Society. published for the American Astronautical Society by Univelt, Incorporated, 2018.

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Olson, Nathan. Cubes. Capstone Press, 2008.

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1922-, Hemmings Ray, and Leapfrogs Limited, eds. Cubes. Leapfrogs, 1986.

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illustrator, Mitter Kathy, ed. Cubes. Magic Wagon, 2012.

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Lewitt, Shariann. 100 cubes. Cantz, 1996.

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America, Cuisenaire Company of, ed. Snap cubes. Cuisenaire Co. of America, 1996.

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Olson, Nathan. Cubos =: Cubes. Capstone Press, 2013.

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Lewitt, Sol. 100 cubes. Cantz, 1996.

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Części książek na temat "CubeSat"

Elsayed, Mohamed Maher, Amir Ashraf, Ahmed Farag, and G. M. Abdo. "Thermal Analysis of an Educational Nano Satellite." In Springer Proceedings in Physics. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-3276-3_15.

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Abstract CubeSats, being small satellites used for educational and scientific purposes, face significant thermal management challenges due to their compact size. This research paper focuses on conducting a thermal analysis of a 1U educational nanosatellite (CubeSat) utilizing Thermal Desktop and SINDA/FLUINT software. The study involves the development of a detailed 3D thermal model of the CubeSat using Thermal Desktop software, followed by thermal simulations using SINDA/FLUINT software. By evaluating the CubeSat's thermal performance under various operating conditions, the analysis aims to i

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Welle, Richard P. "Overview of CubeSat Technology." In Handbook of Small Satellites. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-20707-6_3-1.

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Welle, Richard P. "Overview of CubeSat Technology." In Handbook of Small Satellites. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-36308-6_3.

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Suhadis, N. M. "Statistical Overview of CubeSat Mission." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-4756-0_50.

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Brandon, Carl, and Peter Chapin. "A SPARK/Ada CubeSat Control Program." In Reliable Software Technologies – Ada-Europe 2013. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38601-5_4.

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Welle, Richard, Siegfried Janson, Darren Rowen, and Todd Rose. "CubeSat-Scale High-Speed Laser Downlinks." In Proceedings of the 13th Reinventing Space Conference. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-32817-1_2.

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Eastwood, Jonathan, and John Bellardo. "HeL1oNano: The first CubeSat to L1?" In Proceedings of the 13th Reinventing Space Conference. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-32817-1_6.

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Alqam, Muna, and Samir Al-Busaidi. "Controlling Robot Through Satellite: Telesurgery or Remote Surgery." In Springer Proceedings in Physics. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-3276-3_19.

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Abstract Remote surgery is a promising medical technology that has the potential to revolutionize healthcare with the potential to provide life-saving care to patients in remote areas. However, one of the challenges facing this technology is the time delay associated with data transmission over conventional network infrastructures which makes it difficult to perform delicate procedures. CubeSats are a type of small satellite that can be used to overcome this challenge. CubeSats can be used to reduce the time delay by providing a low-cost, high-bandwidth communication link between the surgeon a

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Speretta, Stefano, Angelo Cervone, Prem Sundaramoorthy, et al. "LUMIO: An Autonomous CubeSat for Lunar Exploration." In Space Operations: Inspiring Humankind's Future. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-11536-4_6.

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Kelley, R. L., and D. R. Jarkey. "Cubesat Material Limits for Design for Demise." In Space Safety is No Accident. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-15982-9_55.

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Streszczenia konferencji na temat "CubeSat"

deLoughery, Tyler J., Clayton D. Lauzon, Kyle H. Sims, John Weber, Wahab Almuhtadi, and Ross Cheriton. "CubeSat Astrophotonics: Lower cost, space-based optical astronomy using photonic integrated circuits." In Integrated Photonics Research, Silicon and Nanophotonics. Optica Publishing Group, 2024. http://dx.doi.org/10.1364/iprsn.2024.iw3b.4.

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CubeSats are low-cost, space-based platforms for sensing instrumentation, where limits on size, weight and power limitations favour using photonic integrated circuit. We explore the design and performance of a proof-of-concept astrophotonic CubeSat for optical astronomy.

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Rose, Todd S., Ariel Berman, Nicolette Werner, et al. "CubeSat optical crosslink." In Free-Space Laser Communications XXXVII, edited by Hamid Hemmati and Bryan S. Robinson. SPIE, 2025. https://doi.org/10.1117/12.3046136.

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Skinner, Mark A. "CubeSat Confusion: Further Observations of a CubeSat-Based Pulsed LED Beacon." In 22nd IAA Symposium on Space Debris, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078360-0004.

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Woo, Hyunwook, Octavio Rico, Simone Chesi, and Marcello Romano. "CubeSat Three Axis Simulator(CubeTAS)." In AIAA Modeling and Simulation Technologies Conference. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6271.

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Khan, Muhammad Shadab, Rauno Gordon, Martin Simon, et al. "Development and flight results of TalTech University CubeSat mission." In Symposium on Space Educational Activities (SSAE). Universitat Politècnica de Catalunya, 2022. http://dx.doi.org/10.5821/conference-9788419184405.117.

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Student Satellite program at TalTech, Tallinn University of Technology, Tallinn, Estonia was initiated in 2014 with an aim to impart space technology knowledge to the Estonian students as well as assist towards development of new Space Technologies in Estonia. Two 1-Unit CubeSat named Koit and Hämarik that translates respectively as Dawn and Twilight in Estonian are part of the TalTech Satellite Program. The main scientific mission of the CubeSats was to demonstrate Earth observation and Optical Communication technology. Satellites had two types of cameras, an RGB Camera and an NIR Camera to c

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Lombardo, M. "An overview of the ArgoMoon and LICIAcube flight dynamics operations." In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-138.

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Abstract CubeSats are becoming a reliable alternative for low-cost space applications in deep space, as mission companions or as standalone missions. The use of CubeSats in deep space requires to address many operational challenges, particularly those related to navigation. LICIACube and ArgoMoon are the first two 6U CubeSat missions to the outer space funded and managed by the Italian Space Agency, whose spacecrafts have been developed and operated by Argotec. The flight dynamics operations of both missions were performed by the flight dynamics team of the University of Bologna using NASA/JPL

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Blazquez, E. "Small celestial body exploration with CubeSat Swarms." In Aeronautics and Astronautics. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902813-129.

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Abstract. This work presents a large-scale simulation study investigating the deployment and operation of distributed swarms of CubeSats for interplanetary missions to small celestial bodies. Utilizing Taylor numerical integration and advanced collision detection techniques, we explore the potential of large CubeSat swarms in capturing gravity signals and reconstructing the internal mass distribution of a small celestial body while minimizing risks and Delta V budget. Our results offer insight into the applicability of this approach for future deep space exploration missions.

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Curatolo, A. "A distributed nanosatellite attitude testing laboratory for joint research activities." In Aerospace Science and Engineering. Materials Research Forum LLC, 2023. http://dx.doi.org/10.21741/9781644902677-30.

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Abstract. During the last decades, there has been an increase in the use of satellites of reduced dimensions. Among the others, microsatellites (mass from 11 to 200 kg) and nanosatellites (1 to 10 kg) have been the ones receiving increasing interest from Universities for educational activities [1], [2]. Their reduced cost, complexity and developing time compared to larger satellites make them particularly suitable for student projects. In this regard CubeSats (satellites of standardised dimensions, based on 1 unit, 10x10x10 cm) were developed at Caltech with the goal of having a low cost and f

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Eschelmüller, V., A. Stren, M. Issa, et al. "Development of a CubeSat CLIMBing to the Van-Allen belt." In Symposium on Space Educational Activities (SSAE). Universitat Politècnica de Catalunya, 2022. http://dx.doi.org/10.5821/conference-9788419184405.048.

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Based on its successful CubeSat mission PEGASUS, the University of Applied Sciences Wiener Neustadt (FHWN) is preparing its new CubeSat mission called CLIMB. CLIMB is a 3U CubeSat that will be launched to a low, circular orbit of about 500 km. Using a Field Emission Electric Propulsion (FEEP) system commercialized by the company ENPULSION, the satellite will be lifted to an elliptical orbit with its apogee around 1000 km – well inside the inner Van Allen belt. During its 1.5 yearlong ascent and its operation in the Van Allen belt, the satellite will continuously monitor the space radiation wit

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Watson, Erkai, Nathanaël Durr, Jose-Luis Sandoval Murillo, Markus Büttner, and Pascal Matura. "Simulating Hypervelocity Impacts on Cfrp with a Discrete Element Approach." In 2022 16th Hypervelocity Impact Symposium. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/hvis2022-57.

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Abstract Numerical simulations provide a powerful tool for investigating satellite breakups resulting from hypervelocity impact, and a discrete element simulation method has been shown to be well suited to model the fragmentation that materials undergo upon impact at high velocities. In this paper, we describe new developments to a discrete element simulation method to allow the modeling of orthotropic materials, specifically carbon fiber reinforced polymers which are commonly used in modern satellites. We model carbon fiber reinforced polymers by using different parameters for fiber and matri

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Raporty organizacyjne na temat "CubeSat"

de Vries, Wim. Cubesat Drag Calculations. Office of Scientific and Technical Information (OSTI), 2010. http://dx.doi.org/10.2172/1124870.

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Shiroma, Wayne A., Larry K. Martin, Nicholas G. Fisher, et al. Ho' oponopono: A Radar Calibration CubeSat. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada564129.

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Rossberg, Felix. Structural Design of a NPS CubeSat Launcher. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada490976.

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Akins, Alexander Brooks. Payload Communications Interface for CubeSat Platform: Design Review. Office of Scientific and Technical Information (OSTI), 2015. http://dx.doi.org/10.2172/1209454.

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Belian, Olivia, and Rachel Jones. CubeSat Interplanetary Exploration: A Deep Dive into Nuclear Propulsion and Astrodynamics for Small Satellites. Office of Scientific and Technical Information (OSTI), 2024. http://dx.doi.org/10.2172/2426290.

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Nathan Jerred, Troy Howe, Adarsh Rajguru, and Dr. Steven Howe. DUAL-MODE PROPULSION SYSTEM ENABLING CUBESAT EXPLORATION OF THE SOLAR SYSTEM NASA Innovative Advanced Concepts (NIAC) Phase I Final Report. Office of Scientific and Technical Information (OSTI), 2014. http://dx.doi.org/10.2172/1134415.

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Mastrogiannis, Evangelos. Theoretical and Experimental Validation of a CubeSat's L-Band Communication System. Portland State University Library, 2000. http://dx.doi.org/10.15760/etd.7438.

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Souza, P. Ultrasonic Time-of-Flight Measurements on Binary U-6Nb Cubes. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/15016861.

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Ledbetter, W. B., Matti Relis, and Robert Denson. Feasibility of Producing Large-Sized, High-Strength Motor & Concrete Cubes. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada167993.

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Farber, Steven. Connecting People to Places: Spatiotemporal Analysis of Transit Supply Using Travel-Time Cubes. Portland State University Library, 2016. http://dx.doi.org/10.15760/trec.143.

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