Youngbum Song, Sang‐Young Park, Sangwon Lee, Pureum Kim, Eunji Lee, Jaejin Lee,
... Earth environment. SNIPE mission comprises four 6U size nanosats that perform formation flying to meet the scientific ... formations and adjust the relative distances between the nanosats. Changing the shape and size of the formation ... orbit control epoch, conditions in attitude control of nanosats, limitations of orbit control operation time to secure ... thrust module. The numerical simulations demonstrated that each nanosat satisfied the mission requirements in a Δ V ... formation. • The SNIPE mission comprises four 6U size nanosats. • We designed a formation flying system and validated ...
Tópico(s): Astro and Planetary Science
2021 - Elsevier BV | Acta Astronautica
Chee Khiang Pang, Akash Kumar, Cher Hiang Goh, Cao Vinh Le,
... design and robust scheduling of a nano-satellite (nanosat) swarm is presented for synthetic aperture radar (SAR) ... on the power budget and bandwidth limit of nanosats, the nanosats’ form factor and swarm size are chosen to ...
Tópico(s): Spacecraft Dynamics and Control
2015 - Institute of Electrical and Electronics Engineers | IEEE Transactions on Aerospace and Electronic Systems
Marianna Rinaldi, Federico Cecchini, L. Pigliaru, T. Ghidini, Francesco Lumaca, Francesca Nanni,
... provided that fused-deposition modeling (FDM) is used, nanosats and other structures could be easily produced in ... not demonstrated. This work aimed to realize a nanosat polymeric structure via FDM, including all the phases ...
Tópico(s): Bone Tissue Engineering Materials
2020 - Multidisciplinary Digital Publishing Institute | Polymers
Seokju Kang, Youngbum Song, Sang‐Young Park,
... observe the near-Earth space environment using four nanosats. To meet the requirements to achieve the scientific ... and the initial relative orbits of the four nanosats meeting the formation requirements and thrust limitations of ... the accumulated total thrust required for the four nanosats. If the cross-track formation scenario presented in ...
Tópico(s): Astro and Planetary Science
2020 - Korean Space Science Society (KSSS) | Journal of Astronomy and Space Sciences
Naoufal Raissouni, Samir El Adib, José A. Sobrino, Nizar Ben Achhab, Asaad Chahboun, Abdelilah Azyat, Mohammed Lahraoua,
... pico electronics and computational technologies. More than 1600 nanosats and CubeSats exist nowadays (i.e. 685 nanosats launched, 613 CubeSats launched, 405 nanosatellites in orbit, 321 operational nanosatellites, 71 nanosats destroyed on launch, etc.), with an incredible panoply ...
Tópico(s): CCD and CMOS Imaging Sensors
2019 - Taylor & Francis | International Journal of Remote Sensing
Pablo Ortega, Gema López, J. Ricart, Manuel Domínguez-Pumar, Luís Castañer, J.M. Quero, C.L. Tarrida, Juan García, M. Reina, A. Grás, M. Angulo,
... attitude control system of the Spanish nano-satellite NANOSAT-1B. This device is made of four silicon ... these sensors have already been integrated in the NANOSAT-1B platform that has been successfully launched in ...
Tópico(s): Astronomical Observations and Instrumentation
2010 - IEEE Sensors Council | IEEE Sensors Journal
Marina Díaz Michelena, Ignacio Arruego, Javier Martinez Oter, H. Guerrero,
... the-shelf (COTS) magnetic sensor for the mission NANOSAT-01 and the set of tests that have ... the aerospace industry. The whole system installed in NANOSAT-01 is formed by two biaxial sensors with ...
Tópico(s): Spacecraft Design and Technology
2010 - Institute of Electrical and Electronics Engineers | IEEE Transactions on Aerospace and Electronic Systems
W. W. Weiß, S. M. Ruciński, A. F. J. Moffat, A. Schwarzenberg‐Czerny, Otto Koudelka, C. Cordell Grant, Robert Zee, R. Kuschnig, S. M. Mochnacki, J. M. Matthews, P. Orleański, A. A. Pamyatnykh, A. Pigulski, J. Alves, M. Guêdel, G. Handler, G. A. Wade, K. Zwintz,
... ground. The current mission design consists of six nanosats (hence Constellation): two from Austria, two from Canada, and two from Poland. Each 7 kg nanosat carries an optical telescope of aperture 3 cm ...
Tópico(s): Astrophysics and Star Formation Studies
2014 - Institute of Physics | Publications of the Astronomical Society of the Pacific
Lorenzo Cercos, S. Esteban, José M. Girón-Sierra, Jorge Rivas Barriga, Pedro Domingo de Vicente, Manuel Jerez,
The National Institute for Aerospace Technology NanoSat-1B Earth orbiting satellite uses Sun sensors as part of the attitude determination and control system. The sensors have a truncated pyramidal ...
Tópico(s): CCD and CMOS Imaging Sensors
2014 - IEEE Sensors Council | IEEE Sensors Journal
Óscar R. Polo, S. Esteban, Lorenzo Cercos, Pablo Parra, M. Angulo,
... Attitude Control Subsystem (ACS) of the satellite INTA-NanoSat-1B (NS-1B). This satellite was launched on ...
Tópico(s): Space Satellite Systems and Control
2013 - Elsevier BV | Acta Astronautica
Xiwang Xia, Chongbin Guo, Guoshan Xie,
Most of the low-cost NanoSats, which run on the low-earth orbits and have no severe pointing requirement, usually adopt magnetic-based attitude control scheme as ... task of the attitude control system of the NanoSats is to achieve rate damping and the famous ...
Tópico(s): Spacecraft Dynamics and Control
2018 - Elsevier BV | Aerospace Science and Technology
Gabriel G. Machado, R. Cahill, Vincent Fusco, Gareth A. Conway,
... distances above the surface of a 10 cm Nanosat mock-up. This scenario is chosen as the ...
Tópico(s): Metamaterials and Metasurfaces Applications
2019 - IEEE Antennas & Propagation Society | IEEE Antennas and Wireless Propagation Letters
W. W. Weiß, A. F. J. Moffat, A. Schwarzenberg‐Czerny, Otto Koudelka, C. Cordell Grant, Robert Zee, R. Kuschnig, S. Mochnacki, S. M. Ruciński, J. M. Matthews, P. Orleański, A. A. Pamyatnykh, A. Pigulski, J. Alves, M. Guêdel, G. Handler, G. A. Wade, Arpad L. Scholtz,
... design consists of three pairs of 7 kg nanosats (hence “Constellation”) from Austria, Canada and Poland carrying ... the other, a red filter. The first two nanosats (funded by Austria) are UniBRITE , designed and built ... three-axis attitude control system to stabilize a nanosat with very low inertia. The pointing stability is ...
Tópico(s): Inertial Sensor and Navigation
2013 - Cambridge University Press | Proceedings of the International Astronomical Union
G. R. Swenson, Purvesh B. Thakker, Farzad Kamalabadi, Mathew Frank, Victoria Coverstone, H. D. Voss,
... class called Cubesats and (20-30 kg) called Nanosats have been under development at the University of ... Taylor University has led the development of a Nanosat called TEST, which was designed to study ionospheric ... paper describes the development of these Cubesat and Nanosat systems.
Tópico(s): Space exploration and regulation
2007 - SPIE | Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
Defined for academic purposes (low budget projects), NanoSats become of interest in the government and industry communities, since the deployment of swarms would able to act as a single orbiting constellation, ... of a swirling-micropropulsion system that would permit NANOSATs to be "propulsive-independent". This would allow orbital ...
Tópico(s): Electrohydrodynamics and Fluid Dynamics
2018 - AIMS Press | AIMS energy
Marcos Zayat, Rosario Pardo, G. La Rosa, R. P. del Real, Marina Díaz-Michelena, Ignacio Arruego, H. Guerrero, David Lévy,
Tópico(s): Geomagnetism and Paleomagnetism Studies
2009 - Springer Science+Business Media | Journal of Sol-Gel Science and Technology
Produção Nacional
Fernando de Souza Costa, Ricardo Vieira,
This work determines the preliminary mass distribution of hybrid rockets using 98% H2O2 and solid paraffin mixed with aluminum as propellants. An iterative process is used tocalculate the rocket performance characteristics and to determine the inert mass fractionfrom given initial conditions. It is considered a mission to place a 20 kg payload into a 300 km circular equatorial orbit by air launched and ground launched hybrid rockets usingthree stages. The results indicate total initial masses of ...
Tópico(s): Spacecraft and Cryogenic Technologies
2010 - Springer Science+Business Media | Journal of the Brazilian Society of Mechanical Sciences and Engineering
William Louisos, Alina Alexeenko, Darren L. Hitt, Adis Zilic,
The next-generation of small satellites ('nanosats') will feature masses <10 kg and require miniaturised propulsion systems capable of providing extremely low levels of thrust. The emergence of viscous, ...
Tópico(s): Spacecraft Design and Technology
2007 - Inderscience Publishers | International Journal of Manufacturing Research
J. J. Jiménez, Javier Martinez Oter, V. Apéstigue, Carlos Hernando, S. Ibarmia, W. Hajdas, J. Sanchez-Páramo, M. Álvarez, Ignacio Arruego, H. Guerrero,
A new proton monitor on board NANOSAT-1B—Las Dos Torres (translated: The Two Towers)—and its preliminary results after two years in orbit and its intercomparison to a ...
Tópico(s): Radiation Effects in Electronics
2012 - Institute of Electrical and Electronics Engineers | IEEE Transactions on Nuclear Science
Lance M. Simms, J. G. Jernigan, Benjamin K. Malphrus, Roger McNeil, Kevin Brown, Tyler Rose, Hyoung Sup Lim, S. Eric Anderson, Jeffrey Kruth, J. Doty, Matthew Wampler-Doty, L. R. Cominsky, Kamal S. Prasad, Eric Thomas, Michael Combs, Robert T. Kroll, Benjamin J. Cahall, Tyler T. Turba, Brandon Molton, Margaret M. Powell, Jonathan Fitzpatrick, D. C. Graves, Stephen D. Gaalema, Shunming Sun,
... of its spectrum. The Cosmic X-ray Background NanoSat (CXBN) is a small, low-cost satellite whose ...
Tópico(s): Advanced Semiconductor Detectors and Materials
2012 - SPIE | Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
Laser propulsion offers the potential to become a competitive alternative for the rapid, efficient transport of small satellites from ground into low earth orbit. Based on recent laser propulsion experiments in our laboratory at DLR we studied the mission characteristics for a 50 kg satellite launch. This comprises reflections on the available or required laser power, the transition of the lightcraft through the atmosphere, the laser range, the transmissivity of the atmosphere for the laser radiation, ...
Tópico(s): Spacecraft Dynamics and Control
2004 - American Institute of Physics | AIP conference proceedings
Chad Fish, Charles Swenson, G. Crowley, Aroh Barjatya, Tim Neilsen, Jacob H. Gunther, Irfan Azeem, Marcin Pilinski, R. Wilder, D.M. Allen, Mark Anderson, B.E. Bingham, Kay Bradford, S. Burr, Robert Burt, Ben Byers, J. Elsila Cook, Kathryn E. Davis, Crystal Frazier, Steven Grover, Glen Hansen, Scott Jensen, R. LeBaron, Joshua Martineau, Jeffrey A. Miller, Joel Nelsen, Weston McClain Nelson, Pamela Patterson, Erik Strömberg, Joshua A Tran, Steven R. Wassom, Cameron Weston, Mitch Whiteley, Quinn Young, Justin Petersen, Scott Schaire, C. R. Davis, M. Bokaie, R. Rees Fullmer, Reyhan Baktur, J. J. Sojka, M. D. Cousins,
... from a moving platform. In addition to demonstrating nanosat-based constellation science, the DICE mission is advancing ...
Tópico(s): Astro and Planetary Science
2014 - Springer Science+Business Media | Space Science Reviews
S. Lacour, V. Lapeyrère, L. Gauchet, S. Arroud, Ronan Gourgues, Guillermo Martín, Samuel Heidmann, X. Haubois, G. Perrin,
... compact makes it easy to test through small nanosats missions. Moreover, they are commonly used in the ...
Tópico(s): Astronomical Observations and Instrumentation
2014 - SPIE | Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
Shannon D. Eilers, Stephen A. Whitmore, Zachary W. Peterson,
... being developed to fill a niche application for nanosat scale spacecraft propulsion. The prototype thruster uses safe- ...
Tópico(s): Energetic Materials and Combustion
2013 - American Institute of Aeronautics and Astronautics | Journal of Propulsion and Power
Stephen Widdis, Kofi Asante, Darren L. Hitt, Michael Cross, W. J. Varhue, Michael R. McDevitt,
The next generation of miniaturized satellites (`nanosats') feature dramatically reduced thrust and impulse requirements for purposes of spacecraft attitude control and maneuvering. The present study is a joint computational ...
Tópico(s): Catalytic Processes in Materials Science
2013 - Institute of Electrical and Electronics Engineers | IEEE/ASME Transactions on Mechatronics
Jeremy Straub, Christoffer Korvald, Anders Nervold, Atif Farid Mohammad, Noah Root, Nicholas Long, Donovan Torgerson,
... preliminary design for the Open Prototype for Educational NanoSats (OPEN) demonstration spacecraft, OpenOrbiter, is presented. OPEN is ...
Tópico(s): Satellite Communication Systems
2013 - Multidisciplinary Digital Publishing Institute | Machines
Colin R. McInnes, Camilla Colombo,
... Scholar[3] Janson S. W., "Silicon Satellites: Picosats, Nanosats and Microsats," Proceedings of the International Conference on ...
Tópico(s): Space Satellite Systems and Control
2013 - American Institute of Aeronautics and Astronautics | Journal of Guidance Control and Dynamics
Darren L. Hitt, Charles Zakrzwski, Michael A. Thomas,
... of Defense agencies. More commonly referred to as `nanosats', these spacecraft feature masses in the range of ...
Tópico(s): Plasma Diagnostics and Applications
2001 - IOP Publishing | Smart Materials and Structures
M. Nowak, S. Lacour, V. Lapeyrère, Lester David, Antoine Crouzier, C. Dufoing, H. Faiz, T. Lemoult, PH. TRÉBUCHET,
PicSat is a nanosatellite currently being developed to observe the transit of the giant planet \b{eta} Pictoris, expected some time between July 2017 and June 2018. The mission is based on a Cubesat architecture, with a small but ambitious 2 kg opto-mechanical payload specifically designed for high precision photometry. The satellite will be launched in early 2017, probably on a 600 km Sun synchronous orbit. The main objective of the mission is the constant monitoring of the brightness of Pic at ...
Tópico(s): Inertial Sensor and Navigation
2016 - SPIE | Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE
Daero Lee, George Vukovich, Regina Lee,
Tópico(s): Geophysics and Gravity Measurements
2017 - Springer Science+Business Media | International Journal of Control Automation and Systems