Technical Poster Session 4

Schedule
Wednesday, August 10th
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2022
3:30 PM	A 100 W-Class Water Hall Thruster: System Evaluation for Missions Beyond LEO Aoma Fujimori, University of Tokyo Kento Shirasu, University of Tokyo Daigo Takasaki, University of Tokyo Hokuto Sekine, University of Tokyo Hiroyuki Koizumi, University of Tokyo Kimiya Komurasaki, University of Tokyo Hiroki Watanabe, Pale Blue Yuichi Nakagawa, Pale Blue Utah State University, Logan, UT 3:30 PM
3:30 PM	A 6 DOF Thrust Measurement System and Evaluation of On-Orbit Thruster Performance Isamu Moriai, University of Tokyo Kentaro Yamauchi, University of Tokyo Hiroyuki Koizumi, University of Tokyo Kimiya Komurasaki, University of Tokyo Utah State University, Logan, UT 3:30 PM
3:30 PM	An Intersatellite Ranging and Communication System: Enabling Small Satellite Swarms in Earth Orbit and Beyond Brodie Wallace, University of Colorado Boulder Scott Palo, University of Colorado Boulder Utah State University, Logan, UT 3:30 PM
3:30 PM	CAPE IV Mission Nick Pugh, University of Louisiana Utah State University, Logan, UT 3:30 PM
3:30 PM	Challenge for Lifetime Extension of a 100 W-Class Hall Thruster with Magnetic Shielding Hiroki Kuwabara, University of Tokyo Kento Shirasu, University of Tokyo Hokuto Sekine, University of Tokyo Koizumi Hiroyuki, University of Tokyo Rei Kawashima, University of Tokyo Kimiya Komurasaki, University of Tokyo Hiroki Watanabe, Pale Blue Yuuichi Nakagawa, Pale Blue Utah State University, Logan, UT 3:30 PM
3:30 PM	Characterization of the Perseus Cold Gas Propulsion System Riccardo Mantellato, Technology for Propulsion and Innovation Nicolas Bellomo, Technology for Propulsion and Innovation Francesco Barato, University of Padua Fabiana Milza, Technology for Propulsion and Innovation Daniele Pavarin, Technology for Propulsion and Innovation Margherita Cardi, Tyvak International Alessia Basler, Tyvak International Filippo Corradino, Tyvak International Utah State University, Logan, UT 3:30 PM
3:30 PM	Daedalus Balloon Launch Vehicle: A Universal Platform to Test CubeSat Prototypes at High Altitudes Ali Malik, California Polytechnic State University Ernesto Montes, California Polytechnic State University Utah State University, Logan, UT 3:30 PM
3:30 PM	Design and Optimization of an Autonomous Constellation of Small-satellites for LEO and Beyond Mohammed Irfan Rashed, Korea Advanced Institute of Science and Technology (KAIST) HyoChoong Bang, Korea Advanced Institute of Science and Technology (KAIST) Utah State University, Logan, UT 3:30 PM
3:30 PM	Design Proposal and Realization of an Academic-Nanosat "PEDAGO-SAT" Platform for Aerospace Training Boutte Aissa, Algerian Space Agency Belaidi El Yazid, Algerian Space Agency Utah State University, Logan, UT 3:30 PM
3:30 PM	Development of a Modular Propulsion System for Use in a Deep Space Hybrid Architecture Stephen Mauthe, Benchmark Space Systems Bradley Hoover, Benchmark Space Systems James Brent, Benchmark Space Systems Noah Szczepanik, Benchmark Space Systems Utah State University, Logan, UT 3:30 PM
3:30 PM	Development of University-Friendly CubeSat Bus and Ground Station Architecture Using Software-Defined Radios Jin S. Kang, United States Naval Academy Utah State University, Logan, UT 3:30 PM
3:30 PM	Feasibility Analysis and Performance Study of a Pulsed Solid Propellant Intergrated Propulsion System for Small Satellites Tahir Kanchwala, Florida Tech Utah State University, Logan, UT 3:30 PM
3:30 PM	Flight and Direct to Earth/Space Relay Communication System Architecture for GSFC CubeSat Missions Ethan Abele, Oklahoma State University Serhat Altunc, Goddard Space Flight Center NASA Obadiah Kegege, Goddard Space Flight Center NASA Kaitlyn Ryder, Goddard Space Flight Center NASA Behnam Azimi, Goddard Space Flight Center NASA Michael Campola, Goddard Space Flight Center NASA Kevin Lynaugh, Vulcan Wireless Inc Gianfranco Barnaba, Vulcan Wireless Inc Sabit Ekin, Oklahoma State University John O'Hara, Oklahoma State University Utah State University, Logan, UT 3:30 PM
3:30 PM	HMSIW Based Highly Selective Dual-Band Bandpass Filter for Satellite Communication Keyur Mahant, CHARUSAT Amit Patel, CHARUSAT Utah State University, Logan, UT 3:30 PM
3:30 PM	Lab-Scale Demonstration of High-Safety Chemical Micropropulsion Using Water Vapor and Micron-Sized Aluminium Combustion Masaya Murohara, The University of Tokyo Zhang Rucheng, The University of Tokyo Hiroyuki Koizumi, The University of Tokyo Kimiya Komurasaki, The University of Tokyo Utah State University, Logan, UT 3:30 PM
3:30 PM	Lesson Learned on the Thermal Analysis of the CubeSat K'OTO Using the Finite Element Method Dafne Gaviria-Arcila, National Autonomous University of Mexico Jorge Ferrer-Perez, National Autonomous University of Mexico Rafael Chavez-Moreno, National Autonomous University of Mexico Carlos Romo-Fuentes, National Autonomous University of Mexico Jose Ramírez-Aguilar, National Autonomous University of Mexico Marcelo Lopez-Parra, National Autonomous University of Mexico Utah State University, Logan, UT 3:30 PM
3:30 PM	MBSE Education Curriculum Using HEPTA-Sat Kit Hands-On Program Masahiko Yamazaki, Nihon University Utah State University, Logan, UT 3:30 PM
3:30 PM	Measurement of CubeSat-Scale, Water-Based Propulsion System Thrust Profile Using a DC Motor Jack Brake, U.S. Naval Academy A.J. Gardner, U.S. Naval Academy Brett Brady, U.S. Naval Academy Jin Kang, U.S. Naval Academy Utah State University, Logan, UT 3:30 PM
3:30 PM	Open-Source CubeSat Optical Communication Receiver Erik Halliwell, University of Alberta Joshua Lazaruk, University of Alberta Shayan Khorassany, University of Alberta Steven Knudsen, University of Alberta Utah State University, Logan, UT 3:30 PM
3:30 PM	Optimization of Directional CubeSat Communications Via Attitude Determination August Williams, Old Dominion University Utah State University, Logan, UT 3:30 PM
3:30 PM	Performance Characterization Tests of REGULUS-150-XE Plasma Thruster Matteo Duzzi, Technology for Propulsion and Innovation Marco Manente, Technology for Propulsion and Innovation Fabio Trezzolani, Technology for Propulsion and Innovation Nicolas Bellomo, Technology for Propulsion and Innovation Alessandro Barbato Lorenzo Cappellini, Technology for Propulsion and Innovation Marco Minute, Technology for Propulsion and Innovation Riccardo Mantellato, Technology for Propulsion and Innovation Utah State University, Logan, UT 3:30 PM
3:30 PM	Pre-Flight Training Using Hardware Simulator of AQUARIUS: Water Resistojet Thruster Flying on ARTEMIS-1 Yasuho Ataka, The University of Tokyo Hokuto Sekine, The University of Tokyo Mariko Akiyama, The University of Tokyo Masaya Murohara, The University of Tokyo Hiroki Kuwabara, The University of Tokyo RuCheng Zhang, The University of Tokyo Yuki Jotaki, The University of Tokyo Aoma Fujimori, The University of Tokyo Utah State University, Logan, UT 3:30 PM
3:30 PM	Radiation Tolerant Ethernet Networking for Future Communications in Small Spacecraft Jorge Piovesan, IDEAS Engineering and Technology Alonzo Vera, IDEAS Engineering and Technology James Lyke, AFRL Utah State University, Logan, UT 3:30 PM
3:30 PM	Real-Time Relay of Small Satellite Remote Sensing Data to Tactical Military Operators Robert Zitz, SpaceLink James Schwenke, SpaceLink Rob Singh, SpaceLink Utah State University, Logan, UT 3:30 PM
3:30 PM	System Architecture for a CubeSat DTE Laser Communication System PJ du Plooy, AAC Hyperion Gilles Ackaert, AAC Hyperion G. Witvoet, TNO W. Crowcombe, TNO Utah State University, Logan, UT 3:30 PM
3:30 PM	Test and Evaluation of GRISSOM-1 CubeSat Communication Subsystem Michael J. Bittle, Air Force Institute of Technology Andrew S. Keys, Air Force Institute of Technology Utah State University, Logan, UT 3:30 PM
3:30 PM	Thermal Modeling of FEMTA Micropropulsion System for CubeSat Attitude Control Florian Alexander Hoeft, Karlsruhe Institute of Technology Steven Pugia, Purdue University of Aeronautics and Astronautics Alina Alexeenko, Purdue University of Aeronautics and Astronautics Utah State University, Logan, UT 3:30 PM

Technical Poster Session 4

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