Digital Commons Network^™

Space Payload For Inertial De-Spin Efficient Effects (Spidee) For Reusable On-Orbit Attachment, Kailia Crowder, David Smith, Raefa Malik, Adam Orris, Simon Lee, Victor Agüero

Small Satellite Conference

The Space Payload for Inertial De-spin Efficient Effects (SPIDEE) is an electroadhesion-based general purpose in-space attachment payload ideally suited for docking, augmentation, mobility, and in-space assembly missions that does not require pre-preparation of the attachment surface.

Built around eTAP^TM (electrical Thin Attachment Pad), SPIDEE supports missions to attach to, detumble, and provide space mobility to defunct satellites and/or rocket bodies. eTAP's low power, reusability, and flexibility make it ideal as an all-purpose attachment and docking technology for the upcoming space challenge of reducing, reusing, and recycling in-orbit debris and/or assets. eTAP adheres to virtually all materials that are used …

Periodic Test Signals For Measurement And Calibration Of Phase Modulated Signals Directly With Spectral Analysis, Brendan Hill, Nazia Mozaffar, Slawan Damman

Small Satellite Conference

Software Defined Radio (SDR) transmitters that employ digital phase modulation can have imperfections in the transmitted waveform that either distort the intended signal or introduce undesired spurious interference. In the case of zero-intermediate frequency transmission, these impairments include amplitude imbalance between the in-phase and quadrature components, quadrature skew in the vector modulator, and local oscillator feedthrough. In the case of heterodyne transmission, where the digital modulation is applied to a carrier offset before digital-to-analog conversion, an undesired image may be present at the vector modulator output. These transmitter impairments can be observed and measured directly with a vector signal analyzer …

The Atlantic Constellation Very High Resolution, A Small Satellite Approach Achieving High-Performance Optical Imagery, Henrique Candeias, Carlos Roldán, Carmen Velarde, Filipe Almeida, Francisco Miguel Ferreira, Gonçalo Aguiar, Gonçalo Correia, Henrique Santos, João Pedro Leitão, John Meyer, Lídia Nogueira, Liliana Baptista, Luis Gomes, Mónica Patrícia Moitas, Pedro Cruz, Pedro Prates, Ricardo Grosso Ferreira, Vasco Amorim, Vítor Botelho, Pedro Coelho, Patrick Silva, João Andrade, Nuno Catarino, André Oliveira

Small Satellite Conference

The Atlantic Constellation (AC) was launched politically by Portugal and Spain in 2021 as an initiative to develop an Earth Observation (EO) satellite constellation capable of delivering multispectral optical imagery at high revisit. The Constellation has evolved over time and is an anchor programme of the Portuguese National Space Strategy. It entails optical VHR satellites as well as SAR observation capabilities. Sharing the same ground and data infrastructure, the constellation will provide coverages at < 1m and images below 50 cm resolution with daily access time based on tasked imaging acquisitions. This constellation will constitute a strategic autonomy asset capable of serving a broad field of sectors, such as Defence, Maritime, Agriculture, Security and Disaster monitoring. As the leader of the VHR space segment component of the AC, and its main industrial partner, N3O faces diverse technical and programmatic challenges. The major challenge arises from the growing commercial demand for rapid access to orbit, which shortens the development and integration timelines imposed by customers. This demand leads to wider adoption for off-the-shelf components. The VHR satellites are a product of this philosophy. One of the major drivers is tailoring the mission requirements to accommodate what standard VHR payloads and small satellite platforms in the market can offer, and what their interfaces can support. Another challenge is maintaining a low orbit altitude, due to limited low thrust system and power capabilities that keep cost and complexity manageable, while ensuring the target 50 cm Ground Sampling Distance (GSD) and fulfilling the updated space debris regulation to decay within 5 years. Moreover, these commercial space products do not always follow standard processes and specifications (e.g. ECSS, MIL), making co-engineering effort and heritage knowledge key for satellite design and verification activities. Opportunities for rideshare and small satellite launch service providers are growing, together with the diverse market on Ground Stations services. Lastly, the development of dedicated in-house facilities and planning for the assembly, integration and test (AIT) phase of the VHR satellites, built from scratch, and based on space industry best practices and standards, all combine to make this one of the most ambitious space programmes ever carried out in Portugal.

The Development Of Dwts (Doppler Wind Temperature Sounder) Climatology Missions For Earth And Mars, Marcus S. Murbach, Alejandro Salas, Arwen Davé, Malachi Mooney-Rivkin, Avery Brock, Kwabena Boateng, Ali Kashani, Larry Gordley, Benjamin Marshall, Joe Gubeli, Amanda Cook, Donald Banfield, Anthony Colaprete

Small Satellite Conference

The Doppler Wind and Temperature Sounder instrument (DWTS) is a unique atmospheric instrument being developed by Global Atmospheric Technologies (GATS), NASA and NOAA. Invented by Larry Gordley/GATS, it is a mid-wave infrared camera paired with a nitrous oxide (NO) cell, which acts as a spectral filter. Wind velocities and kinetic temperatures in the stratosphere and lower thermosphere are extracted by measuring the induced Doppler shift and Doppler broadening of emissions as they pass through the DWTS field of view. Eventually, the use of 3 gas cells(N2O, CO2) would complete the complement such that 20-200km during the day or night could …

A Ground System Framework For Operating Satellites In Very Low Earth Orbit, Kashyapa Naren Athreyas, Bryden Cho, Xiaohua Zhang, Wee Seng Lim

Small Satellite Conference

In the space industry, the space-segment and ground-segment work in tandem to effectively and safely control satellites, execute its intended missions, and obtain meaningful data. In recent years, the space industry has been exploring Very Low Earth Orbit (VLEO) for the following advantages: (a) reduced satellite traffic, (b) increased revisit frequency, (c) shorter communication distances, and (d) closer Earth observation points. However, the exponential increase in atmospheric density and gravitational forces, combined with shorter operational response times to critical events, poses significant challenges for satellite operations. While satellite design should ensure appropriate system sizing and requirements to address these issues …

Laser Crosslink Experiment: Post-Mission Review, Sean Stanko, Dan Frey, Jose Ruvalcaba, Sean Burk, Damian Klaren, Dmitriy Obukhov, Barry Tidmore, Jason Bousquet, David Wayne, Nathan Barnwell, Galen Cauble, Kevin Book, Ben Laxton, Grant Webster, Stan Volchenok, David Sadowski, David Palmer

Small Satellite Conference

The Laser Crosslink Experiment (LaCE) was a Low Earth Orbit (LEO) microsatellite mission that flew between March 4, 2024, and May 18, 2025. LaCE was a two-CubeSat, multi-payload mission developed by Naval Information Warfare Center Pacific (NIWC). Its major payloads included the CACI Skylight laser communication terminal, the ELROI optical beacon, the Vulcan CSR payload radio, and a newly developed NIWC Tracking, Telemetry, and Command (TT&C) ground operations center. Additionally, LaCE led to the development of the Stratospheric Optical Link Demonstration (SOLD) high-altitude balloon experiment, a companion mission which demonstrated the Skylight terminal in the stratosphere as a risk reduction …

Using A Software-Defined Radio Ground Station For A Small Satellite Mission, Simon Gläsner, Victoria Koßack, Mario-Rafael Ionian, Enrico Stoll, Tom Baumann

Small Satellite Conference

In January 2025, InnoCube, a 3U CubeSat was launched with the Transporter-12 mission, becoming the 31st academic satellite of TU Berlin. The technology demonstration mission is the first one at TU Berlin which uses software-defined radio to operate the satellite in the amateur UHF band. The ground station is based on software-defined radio, which has been a vital part of the development of the communication system of InnoCube. Integration into the ground segment is a logical step in the test-as-you-fly philosophy of the mission. The ground segment consists of a SDR which is paired to a power amplifier which includes …

Ai-Driven Mission-Critical Software Optimization For Small Satellites: Integrating An Automated Testing Framework, Vishnupriya S. Devarajulu

Small Satellite Conference

Small satellites (SmallSats) have revolutionized our modern digital infrastructure, such as Earth observation, navigation, real-time communications, and deep space exploration, due to their composable design, effectively reduced cost, and accelerated development cycles. However, SmallSat software must function autonomously, often under limited bandwidth, processing power, and computing resources. Pre-launch techniques such as Hardware-in-the-Loop (HIL), Software-in-the-Loop (SIL) and Unit testing are generally used, but often insufficient to detect errors, timing anomalies, fault propagation, or further telemetry-based degradations. This paper presents a Python-based validation framework influenced by recent testbeds like EIRSAT-1, ITASAT-2, and NOS3, integrating telemetry simulation, synthetic fault injection, resource logging, anomaly …

Attitude Control Of A Floating Satellite (Floatsat) Via Deep Reinforcement Learning, Muhammad Faisal, Dennis Reimer, Sergio Montenegro

Small Satellite Conference

In this work, attitude determination and control (ADC) of a Floating–Satellite(FloatSat)1 through artificial intelligence is proposed. More specifically, Deep Reinforcement Learning (DRL) will be used to generate an optimal control policy for small satellites. This project evaluated an attitude control policy based on deep reinforcement learning using stable–baseline3 (a library which implements the DRL algorithms in PyTorch).² This Artificially intelligent attitude control was realized for a one-dimensional laboratory-based satellite, which is specifically designed to train the students for satellites and their subsystems.

Chantsat-1 Ground Station Planning, Design And Installation - Experiences Gained, Ian Hewitt, Jean French, George Hitt

Small Satellite Conference

Planning, designing, and implementing the ground station for ChantSat-1, Coastal Carolina University’s first small sat mission program, was the first major milestone of the University’s space program. CCU’s ChantSat-1 ground station team presents the experiences gained during the process from inception to completion of the ground station at a liberal arts public University in the southeastern United States with approximately 11,000 students. By sharing both our challenges and successes, our goal is to support others by providing experiences gained in the process.

Efficiency Starts With Lifecycle Planning, Management, And Right-Sizing Process, Brian Simms

Small Satellite Conference

When a program starts, there's a tendency for management or leadership to want to get things moving, to get going, to start doing things. It makes a lot of sense to push forward, but only if everybody understands what "doing things" means. A lot of the time, there's a lack of initial process or clarity about where in a specific process we're starting. Sometimes goals, expectations, and processes don’t reach every member of the team.

In a time when efficiency is being leveraged as a weapon to defund existing efforts, all programs are immediately operating at risk. Programs desperately require …

Hard Disk Drive Reaction Wheel System For Cubesat Architecture, Nidhi Sonwalkar, Venkata Chalamalasetty, Dionna Parina, Parishee Bajaj

Small Satellite Conference

Small satellites have become prevalent within the aerospace industry due to their ability to provide an inexpensive and easily accessible platform for technology demonstrations. Reaction wheels are typically selected for these missions’ attitude and rate control due to their small form factor. Their downside, however, is high cost, upwards of thousands of dollars, which does not align well with the low budget of many small satellites. To address this issue, alternative momentum-actuator technologies can be implemented that, similar to traditional reaction wheels, impart torques for actuation but require much less mass, volume, power, and money. This manuscript discusses the implementation …

Modular Payload Connectivity For Rapid Integration And Testing, Sam Feldman, Noah Gladden, Rahul Rughani, Dave Barnhart

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Optical Telescope Paradigms For High-Performance Cost-Effective Smallsats, Tony Hull, Janina Krieg, Florian Gollier, Dustin Ruth, Thomas Westerhoff, Ralf Jedamsik

Small Satellite Conference

ZERODUR®’s supreme thermo-mechanical stability is enabling for high-performance telescopes, including mirror substrates and even the precision metering structure. For on-orbit high-resolution SmallSat telescopes, tight dimensional control may be passively maintained, even while experiencing continuously changing Solar and Earth thermal view factors. This stability is a vast improvement over implementation in alternate materials like aluminum. ZERODUR®’s thermal and strength characteristics are comprehensively described via ~ 100 scientific publications. Innate stability, decades of spaceborne heritage and expert machining and lightweighting from SCHOTT offers special ZERODUR® cost-effective solutions for SmallSat Telescope Design-to-Cost paradigms, even for constellation level implementation. The latest information for such …

Apophis Cratering Experiment Mission Concept, Ethan Kayser, Tyler Presser, Cristyn Merry, Matthew Givens, Kevin Walsh, Viliam Klein

Small Satellite Conference

Apophis is set to become one of the most extensively studied asteroids in history thanks to the detailed observation campaign of OSIRIS-APEX during its 2029 and 2030 extended mission to the near-Earth object, alongside Ramses which is expected to launch in 2028. To supplement those missions, we propose the Apophis Cratering Experiment (ACE), an impactor mission that leverages OSIRIS-APEX or Ramses as a dedicated observer, during and after the collision, to maximize scientific return at a low cost. In addition to providing significant science return, the mission offers a low-cost opportunity to demonstrate novel SmallSat technologies in deep …

Building Europe’S First Isam Facility – From Concept To Delivery In 12 Months, Mark Heelis, Dimitris Xydas, Alex Goodhand, Jeremy Hadall, Elanor Barber, Rupesh Chudasama, Olivia Markham, Michael Curtis-Rouse

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Peek-Guided Neural Network Pruning For Deployment On Low Swap Hardware, Mackenzie J. Meni, Blake Gisclair, Ryan T. White, Trupti Mahendrakar

Small Satellite Conference

Deploying deep learning models onboard spacecraft is limited by strict size, weight, power (SWaP), and bandwidth constraints. Standard object detection networks like YOLO or Faster R-CNN are too computationally heavy for real-time use in space. We present a pruning framework using PEEK (Probabilistic Explanations for Entropic Knowledge extraction), an entropy-based interpretability method that pinpoints low-information layers for removal. Applied to YOLOv5 for Rendezvous, Proximity Operations, and Docking (RPOD), this approach cuts model size by up to 30% and compute cost by 25%, with only minor accuracy trade-offs—enabling faster, reliable detection on low-SWaP spacecraft platforms.

Qualification Challenges Of An Sadm Using The Slipring Technology, Adrien Guignabert, Flavien Deschaux, Etienne Magnin-Robert, Luc Herrero, Jean-Bernard Mondier

Small Satellite Conference

The SADM-200 (Solar Array Drive Mechanism for 200W) is a new mechanism developed at Comat in order to provide a solution for solar array rotation and power transfer for small satellite applications. This mechanism is designed to be as compact as possible while providing a reliable angular positioning and electrical power transfer from the solar array to the satellite. Robust mechanical guidance and high quality components selection allows an accurate positioning with low angular play while withstanding the tough mechanical and thermal environment faced during launch and in-orbit operations. The development focused on keeping the cost as low as possible …

Optimizing Ground Station Communications Using Multiple Spacecraft Per Aperture In A Ground Segment As A Service Framework, Stefan Vlad Tudor, Giovanni Zanotti

Small Satellite Conference

The increasing deployment of satellite clusters in Low Earth Orbit (LEO) presents new challenges and opportunities for satellite communications, particularly from a Ground Segment perspective. This paper investigates efficient management of multiple ground contacts, in the Ground Segment as a Service context, by leveraging on Multiple Spacecraft Per Aperture (MSPA) technique to maximize connectivity by sharing ground resources to multiple satellites simultaneously.

MSPA is particularly valuable for handling multiple spacecraft in close proximity, such as during the Launch and Early Orbit Phase (LEOP) of rideshare missions, all being supported by same ground segment infrastructure. By enabling simultaneous downlinks through a …

Advancing Real-Time Gnss Data Transmission And Education Through Atak Integration At Cosmiac, Chad Rathbun, Craig Kief, Luis Hernandez, Rachel Hock-Mysliwiec, Michael Starks

Small Satellite Conference

This study showcases COSMIAC at the University of New Mexico (UNM), a leading center for configurable space microsystems and aerospace applications, as it integrates cutting-edge technologies to advance secure and efficient communication systems. Under the AFRL RAPID program, COSMIAC tested a novel architecture combining Azure Orbital Cloud Access (AOCA), the Azure Stack Edge Mini Rugged device, and SpaceX’s Starlink satellite constellation to transmit real-time Global Navigation Satellite System (GNSS) data. The project also leveraged the Android Tactical Assault Kit (ATAK), a geospatial situational awareness tool, to demonstrate the operational utility of advanced data delivery and visualization systems. The results inform …

Autonomous Dual Interchangeable Robotic Arms For In-Space Servicing, Assembly, And Manufacturing, Jonathan Tindall, Michael Daher, Arin Churi, Jake Piccirillo, Anais Mera-Sarnelli, George Serra, Zach Merly, Andrew Dishchuk, Michael Madden, Christian Szczezniak

Small Satellite Conference

The expansion of Low Earth Orbit (LEO) satellite constellations highlights the critical need for In-Space Servicing, Assembly, and Manufacturing (ISAM) to perform novel orbital missions that reduces launch and operating costs and extends mission lifespans. Existing space robotic systems are too expensive, large, and specialized for many ISAM applications in LEO. A small-scale twin robotic arm system that features interchangeable end effectors enhances future ISAM mission capabilities. This robotic arm system leverages smaller, low-cost, arms to perform precise autonomous operations, including satellite repair, repositioning, and recovery. Initial designs and analysis show the arms to be 62% smaller in length and …

Chantsat-1: A First-Time University's Experience In Small Satellite Development, George Hitt, Jean French, Juliana Harding, Ian Hewitt, Louis Keiner, Michael Woodle

Small Satellite Conference

ChantSat-1, Coastal Carolina University (CCU) High Altitude Nadir-pointing Satellite-1, is the first smallsat mission envisioned by our primarily undergraduate university. Capacity development to support mission planning over 18 months has integrated a range of interdisciplinary stakeholders while capturing the attention and imagination of students. The mission’s primary payload will be a multispectral camera for remote sensing of South Carolina’s coastal blackwater rivers, estuaries, and adjacent ocean shelf waters. The resulting coastal habitat mosaic supports ecologically important food webs and related economic and cultural engines of regional growth, while being uniquely vulnerable to the combination of natural episodic climate-related events combined …

International Space Cooperation Between Japan And Paraguay, Shinsaku Nakamura, Alejandro Roman, Kei Sato, Yoshinori Kobayashi, Akie Koga, Atsushi Kimura, Adolfo Jara, Osvaldo Almirón

Small Satellite Conference

Space Agency of Paraguay (AEP) has an ambitious goal to achieve an initiative for developments, operations and utilizations of small satellites in Latin America. Authors collaborated to enhance Paraguayan space programs on socioeconomic benefits through 3 items: 1) providing a technical transfer program about small satellite developments, including Paraguayan 2nd small satellite, GuaraniSat-2 Engineering Model tests in Japan; 2) creating a flood hazard map and designing inter-sectional framework for evacuation planning as a satellite data application on disaster management; and 3) developing soybean monitoring systems through multiple optical satellite data analysis and combining weather information with agricultural and Livestock minitries …

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

Poster presented during the 2025 SmallSat Conference.

Orbital Decay Analysis Of Uae Nanosatellites In Low Earth Orbit, Bassam Alfeeli

Small Satellite Conference

Given the continuous efforts in the United Arab Emirates (UAE) to develop its local capabilities in space technology through the deployment of nanosatellites (cubesats) in Low Earth Orbit (LEO), understanding cubesats orbital dynamics and decay patterns is crucial for both future mission planning and space debris management. This study investigates the orbital decay characteristics of cubesats deployed by the UAE in LEO. We analyzed the orbital decay rates of seven UAE cubesats namely Nayif-1, Mysat-1, Meznsat, QMR-KWT, Ghalib, Dhabisat, and Light-1 by examining observational data, orbital parameters, and environmental factors. The results offer insights into the effectiveness of current satellite …

Orbitcare: A Universal Autonomous In-Orbit Platform For Manufacturing, Servicing, And Debris Mitigation, Rohan Chandratre, Vishish Behera, Anushree Manwatkar, Aruma Kushwaha, Sneha Gayen

Small Satellite Conference

OrbitCare is a proposed orbital infrastructure enabling scalable, sustainable, and cost-effective in-space servicing, manufacturing, and assembly through a modular system architecture comprising an Orbital Manufacturing Hub (OMH) and a fleet of free-flying WorkSat servicing satellites, all integrated via a standardized Servicing Interface Standard (SIS). This paper presents the technical architecture, subsystem design, trade studies, use cases, and development roadmap for OrbitCare. The motivation stems from the current lack of persistent infrastructure in orbit, which renders satellites single-use assets with limited repair or upgrade capabilities. OrbitCare addresses this by combining a permanent hub with reusable robotic satellites to extend spacecraft lifespans, …

Small Satellites, Big Impact: Advancing Space Innovation From Earth To Orbit With The Catapult’S Isam Test Facility, Dimitris Xydas, Oliver Knappett, Lewis Gray, Alex Goodhand, Jeremy Hadall, Michael Curtis-Rouse

Small Satellite Conference

The In-orbit Servicing Assembly & Manufacturing (ISAM) Test Facility at Westcott, UK is a testbed providing realistic environmental conditions for orbital operations here on Earth, with the primary objective of accelerating the readiness level of emerging ISAM technologies and reducing the time to market for commercial space systems. As a result of continuous feedback from campaigns, the Facility has seen recent upgrades to both infrastructure and capabilities, which has created a unique operational environment that acts as an enabler for space activities in the UK and internationally. Moreover, as a constantly evolving system, it is uniquely positioned to adapt to …

Reaching Higher Orbit - A Quick Guide For Exploration Beyond Leo, John Carrico, Mike Loucks, Alisa Hawkins

Small Satellite Conference

Poster presented during the 2025 SmallSat Conference.

Grotifer: A Compact Three-Dimensional Electric Field Instrument Suitable For Small Spacecraft Constellations, Scott Candey, Solène Lejosne, David Auslander, John W. Bonnell, Tatsuyoshi C. Kurumiya, Neli Montalvo, David Pankow, John G. Sample, Van Shourt, Orion V, Van K. Vu, Joshua Zhou

Small Satellite Conference

Existing double probe instruments cannot make equally accurate measurements of all three components of the DC and low frequency E-field. The spin axis booms on spinning spacecraft must be much shorter than spin plane booms and the resulting uncertainty in the spin axis is usually greater than the measured value.

Arizona Dust: Students Advancing Climate Science With Cubesat Technology, Haile Brown, Theodore Courtois, Alyssa Armstrong, Abraham Phillips, Mckayla Morgan, Isabella O'Brien, Aaron Wall, Harrison Constance

Small Satellite Conference

ARIZONA DUST (Arid Region Infrared Zone Observation of Notable Arizona Desert Urban Storms and Temperatures) is a student-led mission team of 25 out of Arizona State University with the goal to understand how Earth’s climate is evolving and why. The 6U CubeSat ‘Dusty’ will orbit at a 400 km altitude in a non-sun synchronous orbit with a 40^° inclination designed to pass over Arizona (as well as Australia). The mission is designed to study monsoon and dust storms to enhance understanding of their effects on temperature as they relate to global climate change. With the orbital path also crossing …