Digital Commons Network^™

A Radio Payload For In-Space Sub-Terahertz Communications, Andrew Benincasa, Sergi Aliaga, Albert Diez-Comas, Josep Miquel Jornet

Small Satellite Conference

This paper presents the first fully integrated design of a CubeSat-compatible sub-terahertz (sub-THz) radio payload for in-space communications at 225 GHz. Addressing the growing congestion in traditional RF bands and the limitations of Free Space Optical systems, the proposed system leverages recent breakthroughs in compact high-frequency front-ends, horn antenna arrays, and RFSoC-based digital processing to unlock multi-GHz bandwidths in the underutilized sub-THz spectrum. A detailed feasibility study confirms link closure from low Earth orbit using state-of-the-art components, and the payload’s architecture is engineered for real-time high-speed uplink/downlink under stringent CubeSat size, weight, and power (SWaP) constraints. The proposed payload will …

4096-Element Ka-Band Deployable Active Phased Array Transceivers In A 6u Cubesat, Hiroki Hayashi, Delburg Mitchao, Yasuto Narukiyo, Sena Kato, Keito Yuasa, Jill Mayeda, Hiraku Sakamoto, Kenichi Okada, Atsushi Shirane

Small Satellite Conference

This paper proposes a 4096-element deployable phased-array transceiver for LEO constellations, operating in the Ka-band frequency range. The system is designed for a 6U satellite platform, with the deployable membrane stored within a 2U volume and deploying to form a 670 mm × 670 mm aperture. The antenna features a central active area of 360 mm × 360 mm, with additional regions allocated for heat dissipation. A 7-layer rigid-flex printed circuit board (PCB) is used in the fabrication for the antenna array. A 256-element phased-array antenna was successfully fabricated on this rigid-flex PCB and demonstrates the feasibility of scaling up, …

Optical Observation Of Mola Cubesat In Orbit Using Ground Telescope, Jeffrey Larsen, Christine Maceo, Isabella Fernald, Matthew M. Knight, Jim Kang, Michael Sanders, Alex Savattone, Giovanni Minelli, Wenschel Lan

Small Satellite Conference

The proliferation of satellites and satellite constellations in orbit, combined with the rapid expansion of telecommunications and wireless “smart” devices on Earth, has led to congestion in the radio frequency spectrum, adversely affecting data transmission and security. Although technological advances in small satellite technology and new commercial models for rocket launches have lowered the barrier for accessing space, the licensing process to use radio frequencies for satellite communications remains an obstacle. Free Space Optical Communication (FSOC) using the near-infrared and visible parts of the unlicensed optical spectrum offers higher bandwidth, faster data rates, and improved security (near-IR). In 2024, the …

Uncoupling Batteries From Eps Design — A Power System For The Modern Era, Andrew E. Kalman

Small Satellite Conference

Space electrical power system (EPS) architectures have often been strongly tied to the voltage of the batteries they employ; the battery operating voltages often dictate the solar cell string lengths and the voltage of the primary buses used for power distribution throughout the spacecraft, as well as internal particulars. This paper presents an alternative space EPS architecture that is independent of battery voltage, and instead, simply treats the connected batteries as a source of power and energy which can be drawn from as desired, and recharged as required. This EPS architecture utilizes a ring bus topology, wherein energy sources feed …

Successful Demonstrations Of The Elroi Satellite License Plate, David M. Palmer, Rebecca M. Holmes Sandoval

Small Satellite Conference

ELROI (Extremely Low Resource Optical Identifier) is a system that attaches a small, cheap, low power, autonomous blinking light to a satellite or other space object to allow it to be unambiguously identified by ground observations using a small telescope. This can provide a resolution to the space object identification problem for future launches at minimal technical and financial costs to the satellite operator. In 2024, two satellites carrying ELROI Space Object Tracking Units were successfully launched on separate rocket launches. As reported here, in both cases ELROI provided the first definitive identification of each satellite, sooner than achieved by …

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 …

Efficient Adaptive Thruster Control Strategies For Nanosatellite Attitude Control, Tian Cilliers, Willem Herman Steyn, Hendrik Willem Jordaan

Small Satellite Conference

This work explores the use of online estimation techniques to enhance advanced thruster-only attitude control strategies. Classical fixed-gain feedback control and newer model predictive control (MPC) based approaches all suffer from reduced efficiency or performance when the system parameters deviate from their nominal values. By incorporating optimal estimation techniques, this can be avoided and deviations from nominal values can be leveraged for fault detection, isolation, and recovery (FDIR).

Specifically, this work investigates the use of extended Kalman filters (EKF) to estimate parameters such as thruster torque and disturbances in real time, using satellite attitude measurements and known control inputs. In …

Finch Eye: The Optical And Optomechanical Design Of A Grism-Based Swir Hyperspectral Imaging Payload For A 3u Cubesat, Iliya Shofman, Mario Ghio Neto, Theaswanth Ganesh, Kenya He, Aidan Armstrong, Ksenya Narkevich

Small Satellite Conference

Crop residue is an important metric used for agricultural land-use monitoring and climate science research. Estimating crop residue coverage is essential to sustainable agricultural practices. There already exist scientific hyperspectral satellites, such as PRISMA and EnMAP, that can be used for crop residue estimation; however, they are very expensive to build and cannot be monopolized by individual farms. This leaves a gap in satellite remote sensing solutions which can be deployed operationally and at the farm scale. We seek to fill this gap by developing a low-cost satellite solution for crop residue estimation. The University of Toronto Aerospace Team is …

Hermes: A Satellite Surrogate Communication Testbed For Ground-Station Validation Using Software Defined Radio And Openc3 Cosmos, Luiz Felipe Bromfman, Gustavo Gargioni, Zach Leffke, Jonathan Black

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

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.

Satellite Navigation With Earth Islands For Scope-1, S. Anand Agrawal, Brandon A. Jones

Small Satellite Conference

Spacecraft optical navigation can deliver autonomous navigation onboard when Earth-based tracking is saturated, obstructed, or impractical. Optical navigation relies on the correspondences between detected and known or mapped features in imagery to extract position and/or velocity, and data-driven methods, which directly leverage collected data to learn, can improve detection performance. This paper presents an initial data-driven Earth-based detection system using islands as landmarks for the SpaceCraft for Optical- based Position Estimation-1 (SCOPE-1) 3U CubeSat, which will be paired on board with a physics-based estimation framework. The system consists of an island detector trained on Earth observation imagery of islands, an …

Rosisat - The Radiation Orbital Shielding Investigation Satellite, Steven Insignares, Jacob Blanton, Colson Walker

Small Satellite Conference

• The Radiation Orbital Shielding Investigation Satellite (ROSISat) is an ongoing 1U CubeSat project designed to study the effectiveness of various materials as shielding against single-event upsets and effects on computer memory modules in Earth orbit.
• ROSISat is a student project managed under the Embry-Riddle Orbital Research Association (ERORA), a registered student organization at Embry-Riddle Aeronautical University in Daytona Beach, Florida.
• It is one of three projects from ERORA presented at this conference, alongside tBEARR and SATLASS.
• ROSISat aims to be the first of ERORA’s projects to be launched and operational in LEO, serving to develop CubeSat flight heritage at ERAU.

An Inter-Satellite Link Experiment On Pearl-1a And Pearl-1b Cubesats, Yun-Ru Chen, Wei-Rong Huang, Chi-Kuang Chao, Jen-Ming Wu

Small Satellite Conference

PEARL (Propagation Experiment using kurz-Above-band radio in Low earth orbit) -1A and PEARL-1B are two 6U XL CubeSats integrated by National Central University (NCU) are designed to perform space-to-earth and inter-satellite radio propagation channel experiments over Taiwan for educational training and scientific research. Both CubSats have the same structures and configurations. Each CubeSat will carry three payloads, an Inter-Satellite Link (ISL) payload, a Compact Ionospheric Probe (CIP), and a Perovskite Solar Cell (PSC) payload. The ISL enables over-the-horizon radio communication experiments, utilizing the Ka-band for both inter-satellite communication and space-to-ground communications. The CIP is an all-in-one in-situ ion sensor developed …

The University Of South Carolina's Journey To The Launchpad, Patrick Bailey, Wout De Backer

Small Satellite Conference

A student team at the University of South Carolina is currently working to address the state’s needs for astronautics to both students and to the economy through collaborative efforts with other state institutions. This paper intends to cover the mission concept formulation, areas of beneficial technology development in space, and mission objectives that are to be accomplished for both human and technical capabilities within the state throughout the mission duration. The mission concept covers using 3D printing in space for on-orbit manufacturing capabilities, and the need for development of a computer vision algorithm and system for small space debris detection. …

Development Of 6u Cubesat Vertecs Utilizing The Birds Bus System, Yukihisa Otani, Jose Rodrigo Cordova-Alarcon, Victor Hugo Schulz, Ryo Hashimoto, Kei Sano, Takao Nakagawa

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Physical Implementation Of Sprint (Space-Based Prioritized Real-Time Inter-Satellite Network Technology), Maleeha Altaf, Dalia Ammar Khodja, Ryan Adams, Sreejith Vidhyadharan Nair, Ronald Fevig

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

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 …