Engineering Commons^™

831sat: A Cubesat Subsystem Platform For Space Systems Development Education, Dominic S. Fucile, George Lordos, James Dingley, Kerri Cahoy, Paul Fucile

Small Satellite Conference

The CubeSat standard has become one of the most popular frameworks for co-curricular and extracurricular student satellite projects, yet its integration into formal curricula for space systems engineering remains limited.

Accessibility concerns:

• Students encountering satellite design for the first time face a learning curve when working with flight-representative hardware.
• Time constraints of undergraduate semesters limit the technical depth covered in a single course.
• Existing educational platforms often lack subsystem flexibility and fidelity needed to deliver an authentic systems engineering experience.

Presented is the 831Sat, a custom single board platform that provides core satellite subsystems:

• Central Processing Unit
• Electrical Power System …

Design And Implementation Of A Semi Automated Uhf Ground Station For Small Satellite Missions: A Case Study From India, Binoop Joseph, Vinayak Manoj, Thomas Francis, Madhav Vinod, Nikhil Jacob, Salih Majeed, Prajin I. R., Meghana Suresh, Salman Al Fariz K., Sijo George, Anish Chandra B. S., Anamika Kamath, Anjay Sudesh, Anurag Reghu, Aravind M. B., Manu Mohan, Ashfaque K. P., Amal Chandran

Small Satellite Conference

Mission success ultimately depends on reliable telecommand and telemetry links between spacecraft and Earth. For small satellites operating under tight power, size and link margin constraints, a technically robust and regulation compliant ground station is a mission critical enabler rather than an afterthought.

This poster presents a case study of a semi automated UHF ground station designed, built and commissioned by HEX20 in Thiruvananthapuram — one of the earliest privately owned and operated satellite ground stations in India — covering the hardware signal chain, the tracking and decoding software stack, integration and calibration, and the regulatory path to operation.

Modeling Liquid Propellant Slosh Disturbances For Small Satellite Attitude Control, Phillip Miret, Nathan Cole, Robert E. Zee

Small Satellite Conference

Objective:

Develop and optimize a reduced order spring-mass-damper (SMD) analogue of propellant slosh using computational fluid dynamic (CFD) analysis. Evaluate the efficacy of generating feedforward compensation terms using the SMD model to improve attitude control performance during rapid spacecraft slews.

Schott Options For Efficient Design-To-Cost Zerodur® Optical Assemblies With Established Supply Chain Reliability, Florian Gollier, Jesse Bonfeld, Dustin Ruth, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

The Quantum Cubesat: A Perspective For Quantum Technology In Orbit, Natalie Pearson, Andrew Kelly, Curtis Talbot, Colin Aitken, Kevin Quillen, Sandy Provan

Small Satellite Conference

Motivation

The ability to measure, control and exploit quantum effects has shown significant potential to outperform classical devices across a variety of applications in computing, sensing and communication. However, quantum devices today typically depend equipment that is large, heavy, expensive and delicate. Bringing quantum capability to space requires a relentless focus on miniaturisation, ruggedisation and applicability. Focusing engineering efforts on the most promising technologies to realise their benefits in orbit is a crucial step in this process.

Gigabit Ethernet Satellite Bus For Smallsat Applications: Standardizing Cots-Based High-Speed On-Board Data Communication, Lucas Felderhoff, Mathias Reibe

Small Satellite Conference

The satellite architectures of modern missions underline the increasing need to simplify and standardize on-board data buses. This requirement becomes more critical as missions demand higher data rates and greater flexibility.

Validation Of A Modular Adcs Architecture For Small Satellites, Saish Sridharan

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

Satellite Autonomous Launch Assembly (Satlass): Cold Gas Propulsion System Testing, Anthony Todisco Jr., Jaden Caradine, Justin Della, Essence Howard, Colin Mccaughey, Andrew Hawks, Alexander Kushto, Javier Narvaez, Gabriella Colon O'Hara, Franyerson Lopez Ochoa, Elizabeth Ptak, Diana Tormo, Francisco Crespo Cutillas, Sean Crouse, Lary Finberg

Small Satellite Conference

Project SATLASS plans to become one of the first cold gas propelled CubeSat Deployers used. Using Nitrogen gas, SATLASS will be able to place multiple CubeSats into customizable orbits autonomously. A modular housing unit will allow for 3-1U CubeSats to 1-3U CubeSat to ride along with SATLASS through Low Earth Orbit.

4dof Steam Propulsion System For 1u Cubesats And Larger, David Hinkley, Jonathan Cheng, Susan Ossareh, Jeff Asher, Logan Fernandez, Brenda Valdez, Bhargav Nagarajan, Aryan Jafari, Stephen Samples

Small Satellite Conference

Aerospace developed a warm gas water vapor propulsion system for the OCSD-A mission in 2015 and redesigned it for the AeroCube-10 mission in 2019. Those were single nozzle systems. The 2019 mission performed reliably so this design is an evolution to 5 thrusters. Also new is that the main tank is additively manufactured aluminum so that tubing can be embedded and thermal management is easier.

Advanced Avionics: Low Swap Hpsc Box For Space Autonomy, Behnam Azimi, Sun Hur-Diaz, Hossein Mohammadkhan, Michael Romeo, Sean Semper, Alan Cudmore

Small Satellite Conference

Objective: To provide a next-generation avionics system built on NASA's High Performance Spaceflight Computing (HPSC) processor technology.

An End-To-End Optical And Ethernet Networking Architecture For Next-Generation Satellite Constellations, Gianluca Giuffrida, Francesco Falaschi

Small Satellite Conference

• Modern satellites generate ever-increasing data volumes, increasingly challenging traditional RF links. IngeniArs combines very high speed optical links, up to 10 Gbps, with an onboard Ethernet routing fabric
• Optical data is packetized and dynamically routed for onboard storage or processing, or relayed across the constellation from satellite to satellite until it reaches an available ground station
• The result is reduced time-to-ground, increased contact opportunities, and more resilient end-to-end data delivery across the space and ground segments, despite intermittent link availability

Autonomous Onboard Navigation And Mission Planning In A Lunar Near-Rectilinear Halo Orbit, Carl De Vries, Robert Pritchett, Sun Hur-Diaz, Nathan Esantsi, Liam Greenlee, Ben Leser, Mike Romeo

Small Satellite Conference

autoNGC is a core Flight System (CFS) application suite that performs real-time, onboard autonomous navigation, guidance and control (autoNGC)

Lego®-Based Cubesats For Space Outreach, Stefan Brandle, Joshua Brown, Evan Smith, Drew Nye, Sydney Reddy, Twidy Kwae, Kaiya Grzesiak, Matthew Roderer, John Hetz

Small Satellite Conference

Taylor University Computer Science and Engineering is building a satellite having a LEGO®-robotics-based payload.

Mission Goals

• Have university students build a novel ELEO satellite
• Demonstrate viability of LEGO robotics electronics in space for short-term low-altitude missions
• Enhance space awareness by capturing the public's imagination through integral use of LEGO in an actual satellite
• Identify partners willing to provide advice and promote this project
• Create additional pathways for K-12 and university student participation in building satellites and satellite-related projects
• Support other space-education organizations through a high-visibility satellite project
• Continue space outreach efforts in the spirit of the ThinSat project
• ThinSat was …

Magnetic Balancing For Microvibration Reduction In Passive Magnetic Bearings For Smallsat Reaction Wheels, Deckers Niel, Baekeland Mante, Cuypers Cedric, Seiler Rene, Vandepitte Dirk, Delabie Tjorven

Small Satellite Conference

Reduction and mitigation of microvibrations constitutes a crucial field of interest in the research of spacecraft reaction wheels. This applies all the more so in small satellites, where even minimal sources of vibrations lead to imprecision of onboard instruments. To address this, magnetic bearings offer contactless support, and thus prevent several sources of microvibrations that exist in classical ball bearings, for instance the mechanical imperfections in rolling elements. The inherently low stiffness of magnetic bearings also significantly reduces the transmitted forces in reaction wheels. Another advantage of contactless support is its potential longer lifetime because of the absence …

Reacquiring Satellites After Unknown Maneuvers In Sensor Blind Spots: A Physics-Informed Behavioral Framework For Closed-Loop Custody Recovery, Naushad Rahman, Niha Agarwalla, Hardik Patel

Small Satellite Conference

Operational problem

After a maneuver during a sensor blind spot, a pre­-gap catalog state may no longer be operationally sufficient. A null look at GS2 must become evidence for where the object could be­ – and where to task next – before access expires.

Recap: A Study Of Downlink Optimization Methods Using Mms As A Template, Connor Firth, Conrad Schiff, Stephen Kreisler, Alexander Barrie

Small Satellite Conference

Motivations: MMS as a paradigm for downlink optimization

• MMS is a multi-agent mission requiring downlink optimization. ReCAP (Remote Coordination, Actuation, and Planning) assigns ground contacts using auctions.
• Five realistic downlink optimization cases are studied, and the amount of data downlinked is tracked to illustrate ReCAP’s ability to optimize for different criteria.
• ReCAP demonstrates value as a real-time, onboard downlink optimization tool.

Reinventing The Reaction Wheel, I. Penchev, N. Andrada

Small Satellite Conference

Rapid growth of microsatellite missions and constellations in the 10–600 kg class is increasing the demand for scalable, high-performance attitude control solutions. Advanced payloads for Earth Observation, Synthetic Aperture Radar, complex science missions, and geolocation systems require:

• Low microvibration performance
• Precise pointing stability
• High angular momentum capacity
• Reliable across mission lifetimes

Space Inventor is qualifying a new generation of 1 Nms-class reaction wheels optimized for microsatellite platforms. The innovative mechanical design, combined with manufacturing-aware system design, unlocks expanded performance and mission opportunities for microsatellites and constellations.

A Comprehensive Review Of Perovskite Materials For Electronic Device Applications, Md Abdul Kuddus Sheikh, Md Shazarul Islam, Daniel Drane, Hasina Huq

Electrical and Computer Engineering Faculty Publications

Perovskite materials have gained remarkable attention as promising candidates for next-generation electronic and optoelectronic devices owing to their outstanding optical absorption, high carrier mobility, tunable bandgap, and cost-effective fabrication. This review explores the recent progress and future potential of perovskite materials across different categories, including organic-inorganic hybrid perovskites, oxide perovskites, and all-inorganic perovskites, emphasizing their structural diversity and electronic tunability. Special consideration is given to various dimensional perovskites (3D, 2D, 1D, and 0D), where reduced dimensionality provides enhanced stability and unique quantum confinement effects advantageous for device performance. The rapid development of lead-free perovskites is also discussed as an environmentally …

Effects Of Infill Pattern And Infill Density On The Flexural Properties Of Markforged Onyx, Jonathon Tran, Rachel Shubella, Alexander Hunt

Mechanical and Materials Engineering Faculty Publications and Presentations

Fused Filament Fabrication (FFF) enables the production of lightweight polymer composite components with complex geometries; however, the effects of infill geometry on printing accuracy and mechanical behavior of unreinforced Markforged Onyx remains insufficiently understood. This parametric study investigates the influence of four infill patterns (gyroid, hexagonal, rectangular, and triangular) and three infill densities (30%, 40%, and 50%) on the post-print mass, dimensional accuracy, microstructure and flexural properties of Onyx specimens fabricated using a Markforged Mark Two printer. Experimental measurements were compared with Eiger slicing software predictions, and geometry- and mass-based area moment of inertia correction methods were evaluated. The results …

An Operator-In-The-Loop Smallsat Operations Simulation For Classroom Training, Samuil Nikolov, Kaelyn Tindall, Lana Laskey

Small Satellite Conference

Training spacecraft operators through a hybrid environment combining live telemetry, game-engine visualization, subsystem consoles, and real-time anomaly response.

Development Of The Korea's First Hyperspectral Microsatellite Constellation For Local-Scale Methane Monitoring: Narsha, Geuk-Nam Kim, Jinyoung Shin, Museong Park, Sang Hun Lee, Heewon Park, Taemin Kim, Jooin Lee, Dohyun Kim, Insun Jung, Marcin Badowski, Kiyun Park, Jae-Pil Park, Jaemin Hong, Yu-Ri Lee, Sujong Jeong, Alexandra Jercaianu, Pawel Snopek

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Manufacturing Advances For Cost Effective, Large Aperture Monolithic Telescopes, T. Suratwala, R. Steele, G. Tham, J. Ross, J. Johnson, O. Herrera, M. Cahill, D. Bechtold, R. Bechtold, F. Ravizza, J. Cortes

Small Satellite Conference

Space has become increasingly more contested over the last decade, with the proliferation of satellites and space assets that require new levels of Space Domain Awareness (SDA). Space is often described by the US Government as the next warfighting domain. Control, understanding and dominance over this vast domain requires exquisite and complex optomechanical systems.

Lawrence Livermore National Lab’s Space Science and Security Program (SSSP) has developed unique monolithic optics, which are ground-aligned during manufacturing and are nearly athermal. These qualities greatly reduce the complexity of the optical payload when compared to legacy telescope designs. Monolithic optics deliver excellent imaging capabilities, …

Multiclass Satellite Payload For Sar, Leonardo Carrer, Davide Giudici, Fabio Gerace, Paolo Falcone, Davide D'Aria, Giuseppe Leccese, Vincenzo Pulcino

Small Satellite Conference

SAR enables reliable all-weather, day-and-night Earth observation. Conventional SAR missions rely on large satellites, high power and costly development cycles.

NanoSat and SmallSat platforms offer faster deployment and lower mission costs, but face strict mass, volume, power and antenna constraints.

A modular multiclass payload allows the same SAR electronic core to be adapted to different satellite platforms.

Distributed SIMO/MIMO operation shares Radar resources across multiple spacecraft, improving scalability, resilience and revisit time. The proposed architecture enables high-performance X-band SAR missions using compact and cost-effective satellite systems.

Rad-Hard Circuits For Complete System-On-Chip Integration Of Smallsat Electronics On Standard Non-Rad-Hard Cmos Including Finfets, Ignatius Bezzam, Dhandeep Challagundla, Riadul Islam

Small Satellite Conference

1. SmallSat Compute Is Thermally Constrained

• SmallSats are packing more autonomy, sensing, and payload processing into tighter volumes.
• Power budget, heat removal, and radiation reliability constrain sustained on-orbit computation.
• Off-chip shielding increases mass and volume
• Redundancy and guard-banding increase switching energy. 
• This work targets lower heat generation and higher reliability inside the silicon.

Systems Progress Overview Of Rosisat: The Radiation Orbital Shielding Investigation Satellite, Chase Patterson, Jacob Blanton, Jayden Mcdonald, Kylie Nager, Colson Walker, Francisco Crespo Cutillas

Small Satellite Conference

Exposure to space weather in the Low Earth Orbit (LEO) space weather environment poses significant challenges to both the integrity and longevity of orbital hardware, as well as the health of astronauts, driving the necessity for improved means of radiation shielding for future manned and unmanned missions. With a 1U CubeSat formfactor, ROSISat is a planned LEO mission that aims to characterize the radiation shielding capabilities of seven candidate materials. By comparing the shielding performance of each composite and constituent material, ROSISat will place a specific focus on correlating how molecular structure influences radiation shielding. Further, current simulations lack the …

University Ground-Station-As-A-Service: Promoting Space It Education And University Collaboration, Daniel Freburg, Will Lewis, Charles Edamala, Phoenix Alpine

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Validation Of Steering Law For A 4-Variable-Speed Single-Gimbal Control Moment Gyroscope Pyramid Cluster Via Spherical Air-Bearing Testbed, Kai Kuo Liao, Chih Ta Wu, Jen Hao Cheng, Po Hsun Yen, Shang Jung Lee

Small Satellite Conference

• VSCMG: wheel speed is commanded with gimbal rate — the extra DOF lets the cluster slide past singularities.
• HIL: a Helmholtz cage replays the on-orbit field and a solar simulator sets the Sun line.
• This work: HIL validation of a weighted-pseudoinverse steering law, 4-unit pyramid.

Zerodur®: Tailoring Opportunities For Your Thermal Environment And Second-Order Optimum Factors, Jesse Bonfeld, Dustin Ruth, Florian Gollier, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

Experimental Investigation Of "Structured Radio Wave" Propagation Using A Deployable Parabolic Reflector With A Uniform Circular Array, Makoto Ito, Tsukasa Funane, Yosuke Tanabe, Miki Yonehara, Hisatoshi Kimura, Keigo Nakamura, Yasuyuki Miyazaki, Satoshi Ikari, Shinichi Nakasuka, Ayako Torisaka, Koichi Watanabe

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Feasibility Of Failure-Resilient Swarm Formation Flying And Multi-Beam Coherent Apertures In 10000+ High-Density Satellite Swarms, Sumio Morioka

Small Satellite Conference

Direct-to-Device (D2D) communication links satellites directly to ground terminals without large antennas, supporting future Cyber-Physical Systems (CPS) and IoT. Our earlier work [1] showed that a formation of 10,000+ ultra-small satellites, as a coherent phased-array aperture, closes the D2D link budget. This study asks whether the formation can be operated within each satellite’s available power.