Digital Commons Network^™

Satellite Passive Ranging Metasurface Optics For Space Rendezvous And Proximity Operations, Jeremy Harris, Zachary Coppens, Cameron Vo, Addison Long

Small Satellite Conference

Rendezvous and Proximity Operations (RPO) are pivotal in a range of space missions, including satellite servicing, debris removal, and formation flying. Traditional RPO sensor technologies, such as LiDAR, radar, and visual cameras, face limitations in terms of power and size requirements. This work introduces a novel passive ranging sensor based on metasurface optics (meta-optics), designed to reduce power and size requirements while enhancing RPO activities by utilizing a single aperture imaging and ranging sensor. The meta-optic device features subwavelength-engineered structures that encode range information using a rotational, double helix point spread function. This new sensor offers potential for reduced power …

Power Optimization Strategy For High-Power Payloads In Next-Generation Satellites, Atif Mahmood, Ayman Muhammad Abdullah

Small Satellite Conference

Flash Talk presented during the 2025 SmallSat Conference.

Scope-1: On-Orbit Surface Feature-Based Navigation And Timing Mission Overview, Paula Delfin, Lance Lui, Margaret Lambert, Dominic Nguyen, Meenakshi Kalinathabotla, Dylan Mcintyre, Maximilian Roccioli, Riley Vazquez, Yan Zhe Wong, Yulia Meza, Brandon Jones, Renato Zanetti

Small Satellite Conference

The SpaceCraft for Optical-based Position Estimation-1 (SCOPE-1) is a 3U CubeSat developed by the Texas Spacecraft Laboratory (TSL) at The University of Texas at Austin to demonstrate near real-time Position, Navigation, and Timing (PNT) estimation primarily using optical detections of Earth’s islands and archipelagos. The mission adapts algorithms originally developed for lunar crater-based PNT and applies them to terrestrial features for validation in low Earth orbit (LEO). SCOPE-1 features an onboard system combining Mask R-CNN-based surface-feature detection, catalog-based feature identification, and an extended Kalman filter (EKF) to estimate position and timing in near real-time. The SCOPE-1 spacecraft will be built …

Orpheus: A Uk-Led Space Mission To Characterize The Space Domain And Advance Future Concepts For Defense, Kit Grange, Alexander Agathanggelou, Gemma Attrill, Alex Gannon, Christine Mccullough, Graham Routledge, Andy Wells, Andrew Nicholas, Bruce Fritz, Daniel A. Lavigne, Robert Boucher

Small Satellite Conference

The ORPHEUS mission is a collaborative research mission between the UK Defence Science Technology Laboratory (Dstl), the US Naval Research Laboratory (NRL), and the Canadian Defence Research and Development Canada (DRDC) to characterise the space domain and advance future concepts for defence.

The ORPHEUS mission comprises two CubeSats flying in a lead-trail configuration in a near-polar low earth orbit and aims to launch in 2027. This is a follow-on mission to the Coordinated Ionospheric Reconstruction Cubesat Experiment (CIRCE) and Prometheus-2 CubeSat missions that were lost due to a launch failure at the start of 2023, combining and updating the payload …

Canadian Space Agency Satellite Operations For The Quantum Encryption And Science Satellite (Qeyssat) Mission, Tyler Hrynyk, Patrick Irvin, Christian Carrié, Maude Robichaud, Philippe Méhu, Éric Gloutnay, Étienne Boulais, Alexander Koujelev, Lydia Philpott, Alexey Tikhomirov, Stéphane Routhier, Hicham Safoine

Small Satellite Conference

The Canadian Space Agency’s (CSA) Quantum EncrYption and Science Satellite (QEYSSat) mission launching in late 2026 will be the first demonstration of ground-to-space Quantum Key Distribution (QKD) in Canada. For this system, the receiving platform is a microsatellite in low earth orbit and the photon source is hosted in a ground based Optical Quantum Ground Station (OQGS). Together, they will enable the creation and exchange of cryptographic keys, establishing secure quantum communications at a minimum distance of 500 km. In the first year of operations, experiments will be performed to demonstrate QKD as an uplink via Weak Coherent Pulse (WCP) …

Escape, Plasma And Acceleration Dynamics Explorers (Escapade) – Enabling A Low-Cost Mars Mission, Jeffrey S. Parker, Andrew Kohler, Mitchell Rosen, Lauren De Moudt, Robert Lillis, David Curtis, Ellen Taylor, Sasha Courtade, Daniel Cosgrove, Christophe Mandy, Antoine Bichara

Small Satellite Conference

The Escape, Plasma and Acceleration Dynamics Explorers (ESCAPADE) mission will provide a comprehensive picture of how solar wind energy flows through Mars’ unique hybrid magnetosphere to drive ion and sputtering escape. The mission has undergone several transformations to accommodate evolving launch constraints, highlighting its resilience and offering valuable insights for designing low-cost, adaptable Mars missions. This paper describes why and how ESCAPADE has pivoted, how the mission design accommodated the change, and what lessons have been learned. The objective is to illuminate how to design launch resiliency into a low-cost Mars mission.

Acmes: The Next-Generation Of Advanced Lwir Observations Of The Earth, Lucas Anderson, Michael Kirk, Chad Fish, Bruno Mattos, Charles Swenson, Miguel Nunes, Robert Wright

Small Satellite Conference

The Active Cooling for Multispectral Earth Sensors (ACMES) program is an advanced Long-Wave IR (LWIR) remote observation Earth Science Small Satellite mission scheduled to launch in 2026 to a high-inclination 550 km Sun synchronous (SSO) orbit. ACMES will host several novel payloads and technologies, including the Hyperspectral Thermal Imager 2.0 (HyTI 2.0), the Filter Incidence Narrowband Infrared Spectrometer (FINIS), the Planar Langmuir Impedance Diagnostic (PLAID) probe, and the Active Thermal Architecture (ATA) system. ACMES will serve a one-year primary mission focused on technology demonstration, followed by a three-year science-based mission to provide valuable LWIR observations of the Earth’s surface. The …

Lightsheet Anomaly Resolution And Debris Observation (Larado), Andrew Nicholas, Kenneth Marr, Josh Wolf, Charles Brown, Vanessa Kooi, Ted Finne, Scott Budzien, Cosimos Cendo, Ivan Galysh

Small Satellite Conference

Space objects in the size range of 0.1 mm to 3 cm are not currently trackable but have enough kinetic energy for lethal consequences to spacecraft. Small orbital debris poses a risk to most space missions; the detection of this debris requires a combination of a large sensor area and large time coverage. For example, a sensor with a time area product of 3 m²years can make a significant contribution to our understanding of the near-Earth small debris population. Deploying large sensors like physical witness plates is resource intensive, due to their size and weight. The light sheet …

Hitching A Ride On History: Nasa’S Space Launch System Artemis Ii Cubesats, Russell Lane, David Beaman, Courtney Ryals, David Hitt

Small Satellite Conference

In early 2026, NASA will launch the Artemis II mission, the second flight of its Orion spacecraft and Space Launch System (SLS) rocket. Artemis II will be the first crewed flight of the systems and will see four astronauts venture around the Moon as a key step toward establishing a long-term human presence in deep space. The 10-day flight will demonstrate NASA's foundational human deep space exploration capabilities. Launching along with Orion on SLS will be four 12U CubeSats developed through partnerships with space agencies around the world that are signatories of the Artemis Accords. The CubeSats will deploy in …

Navigating The Ezie Path: Insights From A Cubesat's Trailblazing Journey Through Nasa Mission Development, Marc Hoffman, Rebecca Wind-Kelly, Nelli Mosavi-Hoyer

Small Satellite Conference

The Electrojet Zeeman Imaging Explorer (EZIE) is a low-cost, multi-spacecraft mission that seeks to capture the magnetic signature of the powerful electrojet currents flowing within the Earth's upper atmosphere. Equipped with the innovative Microwave Electrojet Magnetogram instrument, three identical 6U CubeSats fly in a "pearls-on-a-string" configuration in sun-synchronous, low Earth orbit, crossing the auroral oval over 8,000 times during its 18-month lifetime. As a NASA-sponsored, Category 3, Risk Classification D mission, EZIE accommodates a higher-risk tolerance and moderate budget while offering a substantial return in science. In less than 40 months of development, the project managed the convergence of sponsor …

Deploying And Operating The 25-Satellite Kinéis Constellation, Challenges And Lessons Learned, Franck Darnon, Anissa Bahri, Silvia Salas, Isabelle Hernandez, Damien Servant

Small Satellite Conference

This Kinéis constellation is made of 25 30kg-class satellites, equipped with electric propulsion. The missions are dedicated to IoT (Internet of Things) connectivity and to AIS (Automatic Identification System) monitoring. The satellites were launched by batches of 5, the first took place in June 2024, the last one in March 2025.

The paper discusses how the Ground Control Segment was developed and validated within a complex system and with strong schedule constraints. The validation plan was designed to rapidly de-risk the challenges due to multi- satellite aspects, to focus on a …

Arctic Weather Satellite - One Year In Orbit, Joakim Kugelberg, Niklas Ahlgren, Enne Hekma, Benjamin Jouanneau, Johan Riesbeck

Small Satellite Conference

The European Space Agency's Arctic Weather Satellite (AWS) Proto-flight Model was successfully launched on August 16, 2024. Based on the OHB Sweden’s Innosat platform, the satellite carries a microwave sounder developed by AAC Omnisys. This paper presents the project execution, which balanced a short development schedule and tight cost boundaries, while ensuring that the mission could provide high quality meteorological data. Being a prototype for the design of the satellites to be deployed in the planned EPS-Sterna constellation, the in-orbit commissioning of AWS is crucial to validate the performance of the space segment.

A key objective of the Arctic Weather …

Reaching Full Operating Capability With The Tomorrow.Io Weather Constellation, Scott Williams, Emma Watson, Jan Wicha, Joe Munchak

Small Satellite Conference

The Tomorrow.io weather constellation leverages advances in small satellite technology and the emergence of affordable rideshare options to provide timely, global weather measurements using a constellation of precipitation radars and passive microwave sounders. The focus of this paper is on the design and deployment of Tomorrow.io’s CubeSats carrying passive microwave radiometers known as Tomorrow.io Microwave Sounders (TMS). The TMS instrument design is based on technology transitioned from the MIT Lincoln Laboratory (MIT LL) with technology insertions to improve performance. TMS will achieve full operating capability (FOC) with 12 satellites in a hybrid mix of sun synchronous and mid inclination orbits. …

Starling 1.5 – Space Traffic Coordination Amongst Autonomously Maneuvering Spacecraft, Theodore Hendriks, Matthew Hejduk, Steven Hu, Scott Miller, Caleb Adams, Nathan Benz, Soon Hwang, Terry Stevenson

Small Satellite Conference

Starling 1.5 is a space traffic coordination mission extension to NASA’s successful Starling swarm technology demonstration. NASA partnered with SpaceX to field and demonstrate a space traffic coordination system that allows different satellite owner/operators to rapidly screen trajectories and either claim or refuse maneuver responsibility for mitigating conjunctions, or close approaches, all without human operators in the loop.

Starlink satellites routinely perform autonomous risk mitigation maneuvers (RMMs) to reduce the probability of collision (Pc) for conjunctions with active satellites and other orbital objects such as debris. The NASA Starling primary mission included an autonomous maneuvering capability, which raised the question …

Development Of An Intervention For Optimizing Values Discussions Between Patients With An Lvad, Their Family Caregivers, And The Healthcare Team, Avery C. Bechthold, Rachel D. Wells, Colleen K. Mcilvennan, Martha Abshire Saylor, Daniel D. Matlock, Jesse Lejeune, J. Nicholas Odom

Sigma Foundation for Nursing Research Grant Reports

This project aimed to characterize how adults living with a left ventricular assist device (LVAD) and their family/friend caregivers engage in values-centered discussions, with the goal of informing future interventions that promote values-centered communication with the healthcare team.

Effect Of Informal Marital Separations On Personal Income Taxation, Carol S. Bruch

Tax Adviser

No abstract provided.

Attitude Control Of A Cubesat For The Lunar Navigation Satellite System (Lnss) Using Thrusters And Reaction Wheels, Hyung-Goo Lim, Hyewon Park, O-Jong Kim

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Code Reuse In Cubesat Projects: Analyzing The Adoption Of Open-Source Software From The Birds Program, Husseinat Etti-Balogun, Victor Schulz, Mengu Cho

Small Satellite Conference

Code reuse is a fundamental principle in software engineering, streamlining development processes and reducing costs. In the context of CubeSat development, open-source software frameworks, such as the Open-Source BIRDS CubeSat (OSBC) software, have the potential to enhance collaboration and accelerate mission deployment. However, the ex- tent to which CubeSat teams adopt and adapt these existing software solutions remains underexplored.

This study examines six CubeSat missions derived from the BIRDS satellite bus, assessing their software development strategies and the degree of code reuse from OSBC. By analyzing project documentation, source code repositories, and developer interviews, we investigate key factors influencing software …

Concluding Cysat-1: A Look At The Final Challenges Faced By Iowa State University's First Cubesat, John Elias, Inés Ahedo García, Sydney Schultz, Matthew Nelson

Small Satellite Conference

This paper discusses an overview of the CySat-1 mission, actions taken between its launch and deployment from the ISS, and issues identified in design that impacted the spacecraft’s performance until its re-entry in early January of 2025. The CySat-1 mission was the demonstration of a software-defined radio (SDR) total power radiometer to survey soil moisture. The successful demonstration of the SDR radiometer would have provided basis for future implementation by the SmallSat community by providing an easily customizable radiometer with increased performance versatility. The CySat-1 mission is part of Iowa State University’s (ISU) Make to Innovate (M2I) program, which is …

Cots Implementation Of Magnetorquer-Only Cubesat Spin Stabilization, Joshua Umansky-Castro, Deemo Chen, Om Deshmukh, Haonan Gong, Nicholas Natsoulas, Mason Peck, Andrew Filo, Alex Burke

Small Satellite Conference

This paper presents the implementation of CubeSat attitude control algorithms on commercial off the shelf (COTS) hardware. Cornell’s Alpha CubeSat seeks to spin-stabilize using only magnetorquer outputs and IMU inputs. Extensive software development and testing is carried out to overcome these hardware limitations. This paper shares tools, techniques, and niche considerations when bringing the control algorithm from simulation to hardware-in-the-loop (HITL) testing with embedded flight software. In-depth approaches for magnetometer filtering are discussed, along with software implementation decisions for safe mission operations.

Cadence-Swans: Continuous Autonomous Detection Enabling Networked Collaboration Explorers Of A Space Weather Anomaly Notification System, Matthew Chang, Kelly Williams, Pragun Bethapudi, Chloe Lau, Giselle Revolorio, Ella Shepherd

Small Satellite Conference

Through the University Nanosatellite Program (UNP), the Bronco Space Lab at Cal Poly Pomona presents Continuous Autonomous Detection Enabling Networked Collaboration Explorers of a Space Weather Anomaly Notification System (CADENCE–SWANS): a pathfinder mission demonstrating autonomous space weather monitoring using a low-latency, onboard radiation notification system. The spacecraft conducts coarse energy spectroscopy in real time to detect elevated radiation levels and autonomously generate notifications, including time-stamped records of detection-to-decision latency.

CADENCE–SWANS uses a novel compact, low-SWaP-C coarse particle energy spectrograph, constructed with varied thicknesses of shielding, to estimate particle energies without requiring precise pointing or expensive particle detectors. This approach enables …

Cubesat Dr3am: A 4u Demonstrative Robust 3d Additive Manufacturing System, Spencer Stowell, Casey Gooch, Taylor Anderton

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Developing A Model-Based Systems Engineering Methodology For Academic Cubesat Missions, Piper L. Kline

Small Satellite Conference

Cube Satellites (CubeSats) have become increasingly popular, particularly in academic settings, due to their affordability, rapid development timelines, and utility as platforms for student training and experimental payloads. Despite these advantages, CubeSat development presents several challenges, including limited resources such as personnel, funding, and time, as well as difficulties in maintaining comprehensive documentation and managing requirements. Student-led projects face additional obstacles, such as inexperienced team members and high turnover rates, which can result in inadequate passing of knowledge. Model-Based Systems Engineering (MBSE) has emerged as a promising approach to address these challenges and improve the efficiency of CubeSat design and …

Development Of A Polarization-Based Optical Communications Ground Station For The Pulse-A Cubesat, Juan Ignacio Prieto Asbun, Leah Vashevko, Mason Mccormack, Rodrigo Spinola E Castro, Ashley Ashiku, Joshua Johnson, Elizabeth Rosario, Kevin Zamudio, Sasha Malysheva, Nusret Efe Ucer, Qihong Wu, Sofia Mansilla, Seth Knights, Logan Hanssler, Mohammad Hassan, Sofia Cavallione, Nguyen Do, Tian Zhong

Small Satellite Conference

The Polarization-modUlated Laser Satellite Experiment (PULSE-A) is the University of Chicago’s student-led mission to demonstrate an optical downlink at a data rate of 1 to 10 Mbps using circular polarization shift keying (CPolSK). PULSE-A comprises a 3U CubeSat bus carrying a < 1.5U optical transmission terminal and a dual optical-RF ground station. The ground station (GS) system consists of the optical ground station (OGS) and the RF ground station (RFGS). The RFGS is responsible for standard communications and control tasks, while the experimental OGS receives the optical transmission from the satellite’s payload.

To perform satellite-to-ground optical communications, the OGS needs to track, receive, and decode the transmitted signal while providing its own beacon, which allows the satellite to track the OGS. These requirements are accomplished by four assemblies within the OGS: tracking, polarization state preparation, signal decoding, and beacon. The tracking assembly collects, condenses, and collimates incoming laser light from the …

Development Of An Open-Source Spacecraft Bus For The Pulse-A Cubesat, Graydon Schulze-Kalt, Robert Pitu, Spencer Shelton, Catherine Todd, Zane Ebel, Ian Goldberg, Leon Gold, Henry Czarnecki, Mason Mccormack, Larry Li, Zumi Riekse, Brian Yu, Akash Piya, Vidya Suri, Dylan Hu, Colleen Kim, John Baird, Seth Knights, Logan Hanssler, Tian Zhong, Michael F. Lembeck

Small Satellite Conference

The undergraduate-led Polarization-modUlated Laser Satellite Experiment (PULSE-A) at the University of Chicago seeks to demonstrate the feasibility of circular polarization shift keyed satellite-to-ground laser communication. Free-space optical communications offer significantly improved data rates and lower power requirements than radio frequency communications for a similar form factor, which makes optical communications of particular interest for future satellite missions as on-orbit data collection rates increase. PULSE-A’s low-cost open-source bus serves as the backbone of the mission and has been designed in tandem with the Payload, with design driven by strict requirements for pointing accuracy, component alignment, power demand, and thermal stability. This …

Development Of Mechanical Ground Support Equipment For Small Satellite Thermal Vacuum Testing, Vincent Côté-Larouche

Small Satellite Conference

Small satellite thermal vacuum tests involve securely mounting a spacecraft in a chamber, providing a representative thermal environment in the absence of convection. This study investigates the design of mechanical ground support equipment for supporting a range of spacecraft masses, from cubesats to ESPA-Grande class satellites of up to 500 kg, inside an existing thermal vacuum chamber. A system of four pieces of equipment is proposed to facilitate thermal vacuum testing, while keeping in mind various considerations such as the laboratory cleanroom environment, available floor space, the load capacity of the chamber rails, the thermal vacuum environment and the human …

In-Orbit Reprogramming Of Satellite’S Fpgas, John Cone

Small Satellite Conference

This document discusses the development of a system to reprogram an FPGA that is located on a satellite in orbit. The new image for the FPGA will be telemetered to the satellite and passed as command data to the subsystem containing the FPGA. The method for reprogramming is robust, verifies that the FPGA image was not corrupted during transmission, and does not rely on the current image or functionality of the FPGA.

Small satellites use Field Programmable Gate Arrays (FPGAs) to interface with the satellite computer and other instruments such as cameras and sensors. These FPGAs are traditionally programmed on …

Navigation Signal Generator For Leo-Pnt On Cubesat Platforms, Ina Jeong, Pilkyo Jeong, O-Jong Kim

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Preliminary Results For Collision Probability Predicted Using Gnss Ephemeris From Cubesats, Weichih Lin, Binson Shih-Pin Lee, Loren Chang

Small Satellite Conference

According to an ESA research report, there are now more than one million pieces of space debris larger than one centimeter in low Earth orbit (LEO) [1]. Conjunction assessment (CA) has been drawing attention in various fields. This study proposes leveraging space borne Global Navigation Satellite System (GNSS) data, including raw pseudorange measurements, to obtain the satellite state vector and covariance for SmallSats or CubeSats. The proposed approach offers the advantage of enabling autonomous CA risk evaluations, while mitigating measurement uncertainties typically associated with ground-based radar systems. Real-time satellite state enables more accurate predictions of future collision probabilities. The COSMIC-2 …

Simulation-Based Evaluation Of Dual-Mode Propulsion Strategies For Small Satellite Collision Avoidance, Michael Harrigan, Charles Cundiff, Joshua L. Rovey, Victoria Coverstone

Small Satellite Conference

As Low Earth Orbit (LEO) becomes increasingly congested, small satellite missions face growing challenges in executing effective collision avoidance maneuvers under limited time and propellant constraints. Dual-mode propulsion systems, combining high-thrust chemical and high-specific impulse electric modes, offer a promising approach to balance rapid response with propellant conservation. This paper evaluates how such systems can be applied to reduce the Probability of Collision (PC) within constrained maneuver windows using sequential chemical-electric burns.

A FreeFlyer-based simulation framework models dual-mode collision avoidance maneuvers across synthetic LEO scenarios. For each case, user-defined mission parameters, such as lead time, PC threshold, and orbital altitude, …