Digital Commons Network^™

In-Orbit Demonstration Of The Vyom-2u: A Green Monopropellant-Based Propulsion System Onboard Isro's Pslv C60 Poem-4, Ashtesh Kumar, Tushar Jadav, Prashant Singh, Rajat Kumar, Sajo George, Sivakami S., Rohit Shanbhag, Neel Gharat, Shubham Singh, Henry Sam, Suman Vadla

Small Satellite Conference

Vyom 2U is a compact 2U green monopropellant propulsion system designed to deliver a total impulse of 1700 Ns. At Beginning-of-Life (BOL) conditions, corresponding to a tank pressure of 24 bar, the thruster can deliver up to 1.1 N with a specific impulse of approximately 250 s, while requiring a peak electrical power of 15 W. At an operating pressure of 14 bar, the propulsion system delivers a thrust of approximately 0.67 N with a specific impulse of about 238 s. This operating point was deliberately selected for in-orbit operations to maintain sub-newton thrust levels compatible with the attitude control …

Initial Flight Test Data Of The Duplex 6u Satellite And The Fppt And Mvp Thrusters, Conor Blount, Magdalena Parta, Chris Young, Andrew Woodruff, Brendan Schulz, Darren King, Curtis Woodruff, Iain Murphy, David Carroll

Small Satellite Conference

NASA’s Space Technology Mission Directorate (STMD) funded CU Aerospace (CUA) to develop and fabricate the Dual Propulsion Experiment (DUPLEX) 6U CubeSat to perform an on-orbit mission demonstration of two new polymer fiber electric propulsion technologies developed by CUA using NASA Small Business Innovative Research (SBIR) funding. Both new propulsion technologies have multiple advantages: they utilize no fluid propellant, no pressure vessel, no valves to clog or leak, and no toxic materials. The 1.7U fiber-fed pulsed plasma thruster (FPPT) uses spooled Teflon filament as its propellant, has extremely high total impulse ( > 29,000 N-s) with high specific impulse ( > 3,500 s), …

First Generation Of Project A.S.P.I.R.E. – A 1u Cubesat Mission For Technology Demonstration And Student Involvement In New Zealand, Shuanghui Zhao, Shunxing Shi, Kristen Lian, Rose Peens-Hough, Arami Peens-Hough, Changrui Wang, Joowon Hwang, Jerry Sun, Edward Sun

Small Satellite Conference

MOTIVATION

A feasibility study conducted at an Auckland secondary school in December 2024 found strong interest in satellite-related learning. Following an outreach presentation, 63 students (Majority aged 15 - 18) completed a questionnaire, with an average interest rating of 4.86/5. The most popular subjects were Orbital Physics, Mathematics, Mechanical Engineering, and Electrical Engineering (fig. 1).

Microsat For Refueling Mission Demonstrator In Vleo, Gyusun Kim

Small Satellite Conference

Recently, active research and technological development have been conducted on various mission application in VLEO(Very Low Earth Orbit) using MicroSat. However, the limited payload accommodation capability of MicroSat poses significant challenges for high optical resolution commercial or national-level practical missions. In contrast, satellites of 2,000 kg in size have performed well in low-Earth orbit for the very high optical resolution missions required so far (e.g., 30 cm-level resolution optical satellites) in 450 km ~ 600 km orbit altitude, but in order to meet the continuously increasing resolution requirements in the future optical imagery market (e.g., 15 cm-level resolution), the optical …

Mission Orientated Flight Software Development: Cubestep, Tirth Thakkar, Howard Lee, Viren Kumar, Maranda Laws, Shridhi Seth, Marco Maggia, Navid Nakhjiri

Small Satellite Conference

Small satellite teams often develop flight software and mission operations separately, leading to software behaviors that drift out of sync with ground procedures. To fix this, we present a co-design approach that directly links mission goals and operational procedures to the onboard flight software architecture. Demonstrated on the CubeSTEP-Cerberus mission using NASA’s F′ framework and FreeRTOS, our system maps mission intent into five constrained software states (Initialization, Safe, Idle, Experiment, and Transmit) guarded by automated health checks. This co-design strategy ensures the spacecraft acts autonomously to preserve its goals while strictly maintaining operator control over critical decisions.

Feasibility Study Of A 3d-Printed Thermally Insulated Battery Compartment For Cubesats, Michal Kolodynski, Konrad Kij, Michal Radawiec

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Citizen Science As A Long-Term Environmental Baseline: Assessing Impacts Of A Small Dam Removal In Montana, Usa, Bethany Blakey, Natalie Bursztyn

Watershed Sciences Student Research

As dam removals increase in frequency across Europe and North America, most research has focused on the impact of larger dam removals, despite the removal of small dams being much more common. There are hundreds of small dams in Montana, USA, and this research investigates impacts on stream ecology and morphology using citizen science data collected over eight years spanning before and after a 2020 small dam removal in Rattlesnake Creek. We analyzed pebble count grain size distributions and aquatic macroinvertebrate biotic indices from 2017 to 2024 to assess changes in sediment transport and macroinvertebrate population as well as evaluate …

A Stackable Multi-Mppt Power Architecture With Paralleled Inputs For Scalable Cubesat Solar Energy Harvesting, Muhammed Syedali N., Anamika A. Kamath, Nithin Krishnan S. S., Ashfaque K. P., Sijo George, Arun P., Jr-Chiun Roger Tsai, Tensae Ali, Jesmin Jose, Athira B. S.

Small Satellite Conference

In traditional CubeSat configurations, the Maximum Power Point Tracking (MPPT) circuit acts as a critical single point of failure because all harvested solar energy is funneled through a single, non-redundant conversion stage. Consequently, the failure of this individual component completely blocks power delivery to the system, permanently stranding otherwise healthy solar arrays and batteries and causing catastrophic mission termination.

This work introduces a modular, stackable solar energy architecture that distributes power conditioning across multiple identical, autonomous modules connected to shared PV and battery buses. By relying purely on analog input-voltage regulation at a common operating point, it eliminates radiation-vulnerable digital …

Lightweight Open Source On-Spacecraft Machine Learning With Mlpack And F Prime, Ryan R. Curtin, Scott M. Gilliland, Sterling L. Peet

Small Satellite Conference

Onboard machine learning is an increasingly important topic in spaceflight systems, as machine learning and AI models are increasingly used for data processing, anomaly detection, attitude control systems, and other predictive applications. However, successfully deploying a machine learning model in a spaceflight computing environment is fraught with difficulty, as spaceflight computing environments are low-resource, but typical machine learning software solutions are implemented in languages like Python, which require an interpreter and other heavyweight dependencies. It is therefore virtually mandatory for any on-spacecraft machine learning to be written with lightweight toolkits that minimize dependencies and resource usage.

We demonstrate a solution …

Nasa Stari Mission: A Formation-Flying Pathfinder For Space Interferometry, Akshat Dubey, Caden Burkhardt, Raven St. Clair, Austin Thomas, Tobey Chang, Shivani Sunil, Jacob Klingler, Bradley Bialke, Hannah Cherry, Adrien Boissy, Yethinder Ragav Lakshmi Kumar, Daniil Voloshin, Michael Meyer, John D. Monnier, James W. Cutler, Ethan Foss, Samuel Y. W. Low, Antonio Rizza, Simone D'Amico, Althea Noonan, Mark Gorrow, E. Glenn Lightsey, Melissa Flores, Alexa Lapinta, Albert Ostoja-Starzewski, Leonid Pogorelyuk, Gautam Vasisht, Kerri Cahoy

Small Satellite Conference

The STarlight Acquisition and Reflection toward Interferometry (STARI) mission is a NASA-funded two spacecraft 8U CubeSat technology demonstrator currently in Phase B designed to advance key capabilities required for future space-based optical interferometers. STARI will demonstrate end-to-end beam transfer by reflecting starlight from one spacecraft to another and injecting the received beam into a single-mode optical fiber when it launches in 2029. Formation flying and transferring starlight at very close proximities (25-200 m) presents GNC challenges such as collision safety, precision position control, and fast, precise beam control. The mission ConOps along with a sophisticated GNC system enables passively safe …

Software Defined Swarms, Nathan Benz, Scott Miller, Jeff Huang, Sonny Hwang, Todd Sarshad, Edmund De La Cruz, Thomas Magesarcher

Small Satellite Conference

The Starling Extended Mission has demonstrated the transformative potential of software-defined architectures in multi-spacecraft swarms. Building on the original Starling mission, which validated autonomous coordination and networking among small satellites, the extended phase focused on adaptability—updating onboard payload software and software-defined radios (SDRs) to enable entirely new experiments without hardware modifications. This capability signals a new approach: spacecraft swarms can evolve post-launch to meet emerging scientific and operational objectives. 

Central to this extension was the deployment of new software enabling two-way ranging and “reverse GPS” source identification using raw radio frequency (RF) signals. Traditionally, ranging and navigation rely on pre-integrated …

Scaling High-Resolution Operations: Implementing Automated Anomaly Response In The Skysat Constellation Via Dove Heritage, Hira Nadeem, Shannon Kyle Cabrera Deleon, Alexander Bauer

Small Satellite Conference

As Planet operates the world's largest commercial Earth observation satellite fleet, the transition from manual mission operations to autonomous systems has become a cornerstone of the ability to image Earth’s landmass each day. Planet operates a constellation consisting of hundreds of Dove satellites, approximately 15 SkySats, and a growing number of Pelican and Tanager satellites. As these on-orbit assets grow in both number and complexity, the move toward heterogeneous fleet management has required a unified approach to automation that spans across diverse satellite architectures concurrently and seamlessly. 

Drawing on the robust heritage of its large-scale Dove constellation, Planet has evolved …

Design Mechanism Framework For Autonomous Small Satellite Constellations – A Newspace Outlook, Mohammed Irfan Rashed

Small Satellite Conference

The increasing deployment of small satellite constellations is driving a transition from isolated spacecraft missions toward distributed and coordinated space operations. However, as constellation size and mission complexity grow, traditional ground-centric operational approaches become difficult to scale due to communication limitations, delayed decision-making, and increased operational workload. While autonomy has been widely explored through onboard algorithms and artificial intelligence techniques, there remains limited focus on how autonomy should be integrated into the systems engineering architecture of constellation missions. This paper presents a Design Mechanism Framework (DMF) for autonomous small satellite constellations that embeds autonomy directly into mission architecture, operational logic, …

Satellite Constellations 2026 - Survey, Trends And Economic Viability, Erik Kulu

Small Satellite Conference

This paper presents the commercial satellite constellation landscape as of Jan 1, 2026. It is based on data from the public NewSpace Index (www.newspace.im), which has tracked commercial constellations since 2016 and contained 456 entries by the end of 2025. 

Many constellation operators have launched initial satellites or small batches, but only a few have reached regular launch rates. Deployment has generally been slower than announced, with many projects scaling back plans or delaying timelines. SpaceX has a significant lead, having launched more than 11,000 Starlink satellites. The next largest commercial operators, Planet and OneWeb, remain well below 1000 satellites. …

Development And Pre-Flight Verification Of The 6u Cubesat Vertecs For Extragalactic Background Light Observation, Ryo Hashimoto, Kei Sano, Takao Nakagawa, S. Matsuura, A. Takahashi, K. Takimoto, K. Tsumura, J. R. Cordova-Alarcon, V. H. Schulz, N. C. Örger, D. Nakayama, E. E. Areda, R. J. G. Rosales, T. Fuse, K. Hamada, Y. Otani, B. V. H. Kumar, K. A. Hil, A. R. S. Islam, T. Tome, Y. Yasudao, C. Narongphun, S. Nakagawa, H. Tanaka, Y. Hirose, Y. Iwaki, A. Ikeda, A. Ojika, Y. Oohara, A. Tsumoto, K. Kurosaki, E. Fukumoto, C. Arakawa, H. Masuno, A. Oho, M. Ebisu, I. Jikuya, M. Cho, H. Masui, H. Matsuhara, N. Isobe, Y. Miyazaki, S. Ikari, Y. Yatsu, T. Wada, R. Funase, K. Hirako, R. Hirose, Y. Ofuji Aoyanagi, T. Goto, T. Hashimoto, V. V. V. Rao, C. Wu

Small Satellite Conference

The extragalactic background light (EBL) (Fig. 1) is the diffuse light arriving from outside our Galaxy. Previous studies revealed that the near-infrared EBL is several times brighter than the integrated galaxy light (IGL).

This excess may originate from the first stellar objects in the early universe or from intrahalo light. Their spectra differ in the visible range (Fig. 2), so the visible EBL is the key to identifying the origin.

Ground-based observations are contaminated by foregrounds such as airglow. We therefore developed VERTECS (Visible Extragalactic background RadiaTion Exploration by CubeSat) to observe the EBL from space.

Ai For Autonomous Operation Of Small Satellite Missions, Lucy Donnell, Reuben Lynch, Charlotte Crawshaw, Karl Buckley, Robert Field, Steven Kay

Small Satellite Conference

UK space industry partners Craft Prospect Ltd (CPL) and GMV deliver an advanced avionics demonstrator which incorporates cutting-edge machine learning (ML) techniques to enhance on-board autonomy for small satellite space missions. The work is funded by the European Space Agency (ESA), and the delivery partners combine expertise in embedded Artificial Intelligence (AI) and space systems engineering to target use cases for on-board autonomy which offer the best gains for a diverse range of mission types including institutional and commercial Earth observation (EO), navigation, scientific, and lunar exploration missions.

Common technical target applications have emerged as underpinning technologies which enable the …

Back From The Dead: Using Stellar Psf Calibration To Recover Operational Value From A Defocused Skysat Telescope, Phillip Linden, Hira Nadeem, Ross Losher, Venkataraman Krishnaswami

Small Satellite Conference

For large-scale Earth observation constellations, such as Planet’s SkySat fleet, a major challenge is mitigating the effects of post-launch optical aberrations, which can render an asset unusable. This paper presents a novel approach to recover operational value from SkySat-C5, which remained excluded from production for 8 years due to significant, uncorrectable focus deficit at launch. Our method leverages stars to calibrate a reliable Point Spread Function (PSF) used in a deconvolution process that restored the camera’s images to a usable level of quality.

Because there is no on-orbit focus mechanism, the only path to restoration is post-processing deconvolution using a …

Probe Cytotoxic And Oxidative Stress Effects Of Nanoplastics On Caco-2 Cells: Insights From Raman Spectroscopy And Machine Learning, Bryan Gustafson, Negar Kosari, Emily Brothersen, Morgan Mosher, Anhong Zhou

Biological Engineering Student Research

Nanoplastics and microplastics have become an increasing ecological and health concern due to their widespread presence in the environment and food chain. In this study, Caco-2 cells were used as an in vitro model of the human intestinal epithelium to investigate the cytotoxic effects of polystyrene nanoparticles and microparticles of varying sizes, concentrations, and surface modification. Oxidative stress and apoptosis were evaluated following particle exposure. Raman spectroscopy, combined with machine learning analysis, was employed to detect and characterize biochemical alterations in the cells. Several peak ratios were selected to cluster data depending on size. A correlation between apoptosis and both …

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 …

Multipoint Sensor Constellations Demonstrated On Spear-1 Using Radstar, Black Box, And Fastbus+, Jeff Dailey, Matt Orvis, John Pugsley, Matt Voss, Hank Voss, Nathan Turner, Dillon Embry, Gretchen Barnes, Mike Schuckel, Nathan Daniels

Small Satellite Conference

NearSpace Launch (NSL) has developed and flown both multipoint sensor constellations and hosted-payload smallsat constellations since 2014, supporting missions for educational, commercial, and government partners. These missions enable distributed, multipoint sensing by combining compact sensor suites with persistent, low-latency satellite links and a common, time-ordered data architecture suitable for constellation operations. Recent flight heritage includes 24/7 space-to-Internet communications and rapid Launch and Early Operations Phase (LEOP) telemetry acquisition to support early identification, commissioning, and anomaly response. Most recently, the Space Power and Energy Advanced Reconnaissance (SPEAR-1) constellation demonstrated this multipoint architecture while maturing advanced power-generation and energy-storage technologies relevant to …

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 …

Design And Performance Of The Active Thermal Architecture Technology For The Upcoming Acmes Mission, Lucas Anderson, Charles Swenson, Miguel Nunes, Robert Wright

Small Satellite Conference

This paper will discuss the basic design, fabrication, and experimental validation plan of the Active Thermal Architecture (ATA), a novel Active Thermal Control (ATC) technology that will be demonstrated on the upcoming Active Cooling for Multispectral Earth Sensors (ACMES) mission. The ATA is an integrated single-phase mechanically pumped fluid-loop (MPFL) thermal control system developed for high-power small-satellite applications. The ATA is constructed using 3D Ultrasonic Additive Manufacturing to co-fabricate the internal thermal transport channels and structural members, enabling direct integration of heat exchangers and fluid pathways within primary spacecraft components. The resulting architecture reduces mechanical interfaces, improves thermal transfer, and …

Event-Driven Spacecraft Operations Demonstrated On Mms, Miles Bengtson, Alexander Barrie, Joseph Patton, Liam Greenlee, Paul Wood, Marcus Piquette, Russell Bjella, Matthew Chang, Joshua Paul

Small Satellite Conference

Operations engineers face the challenging task of capturing high-value science data while maintaining spacecraft health and functionality and responding to a dynamic space environment using limited information. This task is becoming increasingly complex as missions involve increasingly large numbers of spacecraft, target more elusive science signatures, and operate under growing budget and staffing constraints. Conventional pre-programmed time-sequence commands become increasingly burdensome for multi-spacecraft missions and are fundamentally incapable of reacting to rare, transient science events in real time.

To address this challenge, we have developed MEDOS: the Module for Event-Driven Operations of Spacecraft. Unlike machine learning and neural-network approaches, MEDOS …

Intel® Government Technologies Space Products: Leading Edge Compute For Space, Robert Ciccariello, Ricardo Ascazubi, Kyle Dobkins, Nitesh Melwani, Ed Mily, Mike Nassan, Sean O’Neill, Ruchika Singh, Dan Weinstein

Small Satellite Conference

Commercial off-the-shelf (COTS) components are unlikely to meet the environmental survivability and assurance requirements to accomplish mission objectives in the harsh space environment. On the opposite end of the spectrum, developing custom space components on leading-edge technologies will often require multiple contractors and lengthy R&D efforts that significantly increase development costs and timelines. Intel Government Technologies (IGT) is introducing a space product roadmap, focused on space grade systems-in-package (SiPs) designed to address the transition from bespoke legacy architectures to low-SWaP, high-performance processing platforms for on-orbit systems. IGT Space Products are derived from Intel’s latest commercial technology and are uniquely configured, …

Nanouhfcomms Mission Overview, Nazia Mozaffar, Salwan Damman, Ryan Hiser, Lizbeth Durbin, Jose Ruvalcaba, Alejandro Castro, David Sadowski, Dmitriy Obukhov, Brendan Hill

Small Satellite Conference

The NanoUHFComms experiment seeks to demonstrate the ability to detect and correct Doppler offsets caused by the relative high velocity between Low Earth Orbit (LEO) spacecraft and terrestrial nodes. The payload includes a Rincon Research Corporation AstroSDR with external Low Noise Amplifier (LNA) for the receive band and an external power amplifier for the transmit band. The uplink and downlink bands are combined with a diplexer before connecting to a common antenna mounted on the spacecraft. The demonstrations planned for the orbit testing include a relay mode which will detect and correct the Doppler offset of an uplink signal, translate …

Monitoring Spoken Language In Infants And Toddlers Who Are Deaf Or Hard Of Hearing Using The Lena Developmental Snapshot, Monika-Maria Oster, Kimberly A. Peters

Journal of Early Hearing Detection and Intervention

Purpose: This retrospective analysis evaluates the Developmental Snapshot as a language monitoring tool for infants and toddlers with bilateral hearing loss who use listening and spoken language.

Method: Data were obtained from the educational and clinical records of 147 children with bilateral hearing loss. For each child, the LENA (Language ENvironment Analysis) Developmental Snapshot, a standardized online language assessment that relies on parent report, had been completed at least once. When available, scores from other standardized language assessments (PLS-5, CDI, and DAYC-2) were also obtained.

Results: LENA Developmental Snapshot standard scores were characterized by high variability and mean scores in …

A Survey Study On Physiological Hearing Assessment Practice In The Usa, Malina Mangrum, Hasan Saleh, Sangamanatha Ankmnal Ankmnal Veeranna, Kimberly Ward, Charles G. Marx

Journal of Early Hearing Detection and Intervention

Background: In the United States, limited information exists regarding the physiological measures and testing parameters used in infant hearing assessments. To address this gap, we conducted a nationwide survey to identify the types of physiological tests and procedures currently employed by audiologists.

Method: A structured survey was distributed to audiologists across the country to gather information about the auditory tests and recording parameters used in infant hearing evaluations.

Results: Most respondents reported using Auditory Brainstem Responses (ABRs) to estimate infant hearing thresholds, primarily relying on traditional stimuli rather than chirp stimuli. The Auditory Steady-State Response (ASSR) was not widely used …

Measuring Family Involvement In Early Intervention Services For Children Who Are Dhh: A Scoping Review, Marie Martinez, Blair Richlin, Kristina Blaiser

Journal of Early Hearing Detection and Intervention

Background: Family involvement after a child has been identified as deaf or hard of hearing (DHH) is often recommended as “best practice” for Family Centered Early Intervention (FCEI; Szarkowski et al., 2024) and a catalyst for improved outcomes. Defining actions of a family will inform high-quality family support programs. This scoping review aims to explore and document family involvement as well as the current systems of measurement used in early intervention DHH family-centered services.

Purpose: The specific aim of this scoping review was to identify the operational definitions of family involvement and metrics used with families of children who are …

Exploring Speech-Language Pathologists’ Development Of Hearing Loss Health Literacy, Ellie Cooper, Krystal L. Werfel

Journal of Early Hearing Detection and Intervention

Purpose. This qualitative study examined how speech-language pathologists (SLPs) develop hearing loss health literacy through academic training and on-the-job experience. Specifically, it explored SLPs’ perspectives on how graduate coursework and clinical exposure contributed to their readiness to work with children who are deaf or hard of hearing (DHH).

Method. Participants included 48 SLPs with a range of specialty academic coursework and on-the-job experience working with children who are DHH. SLPs were categorized into four groups: with/without specialty academic training in aural (re)habilitation and more/fewer than three years of experience with at least ten children who are DHH. Semi-structured interviews were …

Early Childhood Access To Language Acquisition Services In Arizona, Kendra Benedict, Wendy Steuerwald, Najwa Ghattas, Cheryl Johnson

Journal of Early Hearing Detection and Intervention

This investigation reviewed existing services and gaps for young children who are deaf or hard of hearing (DHH) in Arizona and explored community-based approaches to improve access to language development resources. The study was conducted in two phases, each focusing on different approaches for language acquisition based on surveys of parents and providers. Phase I, completed in 2024, addressed listening and spoken language (LSL) as a methodology for language acquisition while Phase II, completed in 2025, focused on the use of American Sign Language (ASL). Findings from Phase I surveys found that 63% of parents reported using LSL as the …