Digital Commons Network^™

Noaa Nesdis Commercial Data Program Using Small Satellites For Space-Based Environmental Monitoring Data, Marc Gasbarro, Natalie Laudier, Harshesh Patel, Gerald Peltzer, Chunhui Pan

Small Satellite Conference

The National Oceanic and Atmospheric Administration (NOAA) National Environmental Satellite, Data and Information Service (NESDIS) Commercial Data Program (CDP) successfully engages with the private sector to acquire commercial space-based environmental observation data to diversify, streamline, and improve NOAA's observations and to meet NOAA’s mission objectives. The NESDIS CDP manages two lines of effort, the Commercial Data Pilot projects to demonstrate the quality and impact of commercial data on NOAA applications and the Commercial Data Purchases to support operational weather and space weather applications. NESDIS CDP leverages commercial companies’ use of innovative Small Satellite (SmallSat) collection platforms. NESDIS CDP procures data …

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 …

Journal Of Early Hearing Detection And Intervention: Volume 11 Issue 1, Pages 1-80

Journal of Early Hearing Detection and Intervention

No abstract provided.

Odin: Optomechanical Distributed Instrument For Inertial Sensing And Navigation, Mohanad Warrayat, Jackson Dahn, Ramses Miranda, Andrea Nelson, Jeremiah Stoddart, Miguel Dovale, Jose Sanjuan, Felipe Guzman, Daniel Selva

Small Satellite Conference

ODIN (Optomechanical Distributed Instrument for Inertial sensing and Navigation) is a gyroscope-free inertial measurement unit based on a cube of six monolithic fused silica wafers which complete a twelve-axis sensing capability, i.e., three linear, three angular, and six centripetal acceleration measurements. ODIN will fly as a secondary payload on the GRATTIS (Gravitational Reference Advanced Technology Test in Space) mission, slated for launch in February of 2027, led by the University of Florida and funded by the NASA InVEST program. By the end of the GRATTIS mission, it is expected that ODIN will reach an exit TRL-7.

The primary objective of …

Acs3 Results And Lesson Learned, Philip Shih, Olive Stohlman, Ivan Bertaska, Andres Dono Perez

Small Satellite Conference

ACS3 (Advanced Composite Solar Sail System) was a technology demonstration mission for the National Aeronautics and Space Administration¹, to demonstrate the deployment of a solar sail of size 80m² from a new NASA-developed compact deployable composite boom² packaged in a 12U CubeSat. The extended objective of the mission was to perform attitude control and orbit maneuvering. ACS3 was successfully launched on 24 April 2024 local time via Rocket Lab Electron launch vehicle from Rocket Lab Launch Complex 1B in Mahia, New Zealand. Following four months of commissioning operations, the solar sail was deployed on 28 August …

Artemis Cubesats Help Advance Exploration Of The Moon, Mars, And Beyond, Russell Lane, David Beaman, Courtney Ryals, David Hitt

Small Satellite Conference

On April 1, NASA launched the Artemis II mission – the first crewed mission of the Artemis campaign. The nine-day lunar flyby launched on the agency’s SLS (Space Launch System) rocket and had four astronauts test the Orion spacecraft in high Earth orbit and in deep space. Four 12U CubeSats also launched on the mission, housed within the SLS’s Orion stage adapter (OSA). The spacecraft were deployed approximately five-and-a-half hours into the flight, following Orion separation and departure from SLS, as the SLS interim cryogenic propulsion stage (ICPS) and the attached OSA were in a high Earth orbit on an …

The Pandora Smallsat: Overview Of The First Six Months In Orbit, Jessie Dotson, Elisa Quintana, Knicole Colón, Thomas Barclay, Christina Hedges, Ben Hord, Trevor Foote, Jordan Karburn, Pete Supsinkas, Lance Simms, Joe Renaud, Julie Moquin

Small Satellite Conference

The Pandora SmallSat was selected as an inaugural NASA Astrophysics Pioneers mission. The Astrophysics Pioneers program is tasked with performing compelling astrophysics science at lower cost while simultaneously providing space mission experience to early career researchers and engineers. The science goal of Pandora is to study transiting exoplanets and their host stars by collecting long duration, simultaneous visible photometry and near-infrared spectroscopy. This unique dataset will enable Pandora to disentangle the contributions from stellar activity which contaminate the exoplanet spectrum so we can search for water in exoplanet atmospheres.

The Pandora SmallSat successfully launched from Vandenberg Space Force Base on …

Esa Scout Hydrognss Early Mission Results, Martin Unwin, Alex Da Silva Curiel, Ben Stern, Jean-Pascal Lejault, Nazzareno Pierdicca

Small Satellite Conference

The ESA Scout HydroGNSS mission demonstrates a new generation of GNSS reflectometry (GNSS R) capabilities for hydrological climate monitoring from small satellites. HydroGNSS measures soil moisture, freeze–thaw state, inundation, wetlands and above ground biomass by exploiting both traditional incoherent Delay Doppler Maps (DDMs) and several innovative signal types not previously available from spaceborne GNSS R missions. Early in orbit results confirm successful acquisition of signals from Galileo, dual polarisation measurements, coherent complex channel data and reflections at the second GNSS frequency (L5/E5a). These enhanced measurements exhibit stronger than predicted performance and are expected to significantly improve retrievals of climate relevant …

Gray Jay Pathfinder: One Year Of Maritime And Airborne Vessel Monitoring With A Formation-Flying Constellation Of Microsatellites, Erica Peterson, Nicolaas Handojo, Nima Assadian, Jacob Von Chorus, Jeremy Hawke, Andrew Barlow, Sanjeev Narayanaswamy, Abigail Macgillivray, Alex Kiar, Nathan Cole, Robert E. Zee

Small Satellite Conference

Gray Jay Pathfinder (GJP) is an experimental microsatellite constellation that has been designed, built, and operated by the Space Flight Laboratory (SFL), for Defence Research and Development Canada (DRDC). GJP launched in January 2025, and consists of three microsatellites, developed using SFL’s 30kg DEFIANT platform, flying in formation in a sun-synchronous orbit at a 510km altitude. All three spacecraft carry radio frequency (RF) payloads capable of receiving raw spectrum in the VHF, UHF, L, S, and X radar bands. The RF payloads include a combination of in-house designed and COTS antennas, in-house designed antenna front ends, a payload computer with …

Disksat: On-Orbit Performance And Lessons Learned From The Inaugural Flight Of Two-Dimensional Satellites, Darren Rowen, Catherine Venturini, Garrett Kinum, Brian Hardy, Joseph Gangestad, Lisa Toda, Chris Day, Thomas Pridy, Eddson Alcid, Ziba Shahriary

Small Satellite Conference

DiskSat is a novel spacecraft design that uses a disk-shaped form factor, 1 meter in diameter but only 2.5 cm in depth, to provide unprecedented power-to-mass ratio in a nanosatellite and the potential to operate long-term in very low Earth orbit (VLEO). The inaugural flight of four DiskSats launched on 18 December 2025 from NASA’s Wallops Flight Facility on an Electron rocket, which delivered the satellites to a 550-km altitude orbit at an inclination of 45 deg. Developing DiskSat’s two-dimensional form factor presented a myriad of challenges for power generation, thermal management, attitude control, and deployment that could only be …

Design And Development Of A Miniaturized Helmholtz Cage For Cubesat Adcs Testing, Karla Sever, Marko Bosiljevac

Small Satellite Conference

• Magnetic field generation is essential for laboratory testing of a CubeSat attitude determination and control system (ADCS). It supports repeatable evaluation of control algorithms and characterization of onboard magnetometers. Commercial systems are costly, so university labs typically build their own, tailored to their specific needs.
• Building on a review of over twenty university-developed Helmholtz cage designs, several of which were particularly influential to our own design [1-3], this poster presents the design, simulation and early experimental results of our Helmholtz cage, developed as part of the broader ADCS test setup we have been building.

Development Of A Digital Electronic Framework To Manage High Power Systems In Small Satellite Missions, Mariel Serra, Rami Kandela, Bryan Johnston-Lemke, Robert E. Zee

Small Satellite Conference

• As small spacecraft payloads increase in complexity, they introduce the need for higher capacity and reliable power systems.
• The use of radiation tested automotive-grade components offer low-costs, however these parts are less suited to increased power demands, exhibiting signs of on-orbit latch-up.
• A re-design of a Modular Power System’s digital framework is proposed to support more spacecraft loads with minimal computational stress on the electronic processing units.

Distributed Avionics As A Foundational Architecture For Cubesat Constellations And Swarms, Aaron S. Swagei, Ali Guarneros-Luna

Small Satellite Conference

Motivation

CubeSat constellations and swarms require spacecraft that can tolerate subsystem faults without relying exclusively on a single centralized flight computer. Distributing sensing, control, and fault-management authority can improve containment and enable graceful degradation.

Objective

Develop and experimentally evaluate a distributed CubeSat avionics architecture in which subsystem nodes retain local fault-management authority while an F´-based OBC provides mission-level coordination.

The FlatSat is used as a representative spacecraft-level building block for future constellation and swarm architectures.

History Of Aggiesat6: An Undergraduate Mission From Concept To Operations, Garrett M. Stevenson, John F. Connolly

Small Satellite Conference

AggieSat Laboratory (AGSL) is a student-run space vehicle development organization that trains students in systems engineering through hands-on experience in the design, building, testing, and operation of space and space-related systems.

AGSL currently supports 107 members, all but three (3) of which are undergraduates, across eight (8) projects, including an underclassmen shadowing program.

AGSL supports the initiative and learning capabilities of undergraduate members through peer mentorship and the institutionalization of knowledge across its projects to achieve success through a variety of projects.

Integrated Optical/Body-Dynamics Simulations For Pointing, Acquisition And Tracking For The Pulse-A Mission, Juan Ignacio Prieto Asbun, Elizabeth Rosario, Jiayang Xu, Catherine Todd, Robert Pitu, Tian Zhong

Small Satellite Conference

PULSE-A is the University of Chicago’s student-led 3U CubeSat mission to demonstrate a space-to-ground optical downlink at a data rate of 1 to 10 Mbps using circular polarization shift keying (CPolSK).

To avoid costly and ineffective hardware-in-the-loop simulations, we instead present software-in-the-loop simulations designed to qualify our optical and PAT systems. This allows for simulations of the coupled optical systems that include closed-loop corrections and body pointing errors.

Operationalizing On-Orbit Repair: A Conops For Gator Arms Small Satellite Servicing, Anais Mera-Sarnelli, Aimee Dew, Daniel Radu, Chrispher Petersen, Michael Generale

Small Satellite Conference

Mission Definition

• GATOR Arms (Galactic Autonomous Twin Operational Robotic Arms) was designed to provide in-space servicing to small satellites in LEO.
• Small satellites currently have limited servicing options, thus localized component failures can prematurely end otherwise viable missions.
• This poster develops the CONOPS for an operational servicing mission involving on-orbit inspection, repair, refurbishment, reconfiguration, reboost, or repurposing of client satellites for extended missions.
• The representative servicing task is the recovery and reconfiguration of an external deployable such as a solar panel, antenna, or radiator flap.
• GATOR Arms targets a 2-4 year servicing life, end-of-life disposal within 5 years of mission …

Sailing To The Stars Iss Experiment: Results And Conclusions From Light Sail Deployments In Microgravity, Verena Padres, Parishee Bajaj, Venkata Chalamalasetty, Claire Kim, Joshua Umansky-Castro, Dionna Parina, Gabriella Elcsics-Gonzalez, Cameron Goddard, Ethan Francolla, Mason Peck, Andrew Filo, Alex Burke, Olivia Gámez Holzhaus, Heath Mills, Christopher Kelly

Small Satellite Conference

Sailing to the Stars is a mission to test the deployment of free-flying light sails on the International Space Station (ISS). The objective is to understand how different deployer designs affect the stability of both the CubeSat Deployer and the light sail during and after the deployment event. Data from the IMU onboard the deployer and video footage from wall-mounted cameras are used to analyze these dynamics. The findings shall inform the design of future missions that employ this free-flying ChipSat-sail architecture.

The hardware launched with Crew-11 on August 1^st, 2025. Nicole Ayers conducted the experiment on August …

New Frontiers In Diagnosing Equine Lameness, Hyrum Hoopes, Karl Hoopes

All Current Publications

Lameness is one of the most common and expensive health problems seen in horses. Modern technology allows veterinarians to look beneath the surface. Tools such as artificial intelligence (AI), computed tomography (CT), magnetic resonance imaging (MRI), digital radiography (X-rays), nuclear scintigraphy, ultrasound, and positron emission tomography (PET) give clearer, more detailed pictures of what’s happening inside the horse’s leg. Each technology offers different advantages, from identifying uneven movement to revealing hidden damage within bones, joints, or soft tissues. When combined with veterinary visual evaluation, they help pinpoint the cause of lameness faster and more accurately than ever before.

A Proposed Development Process For A Hardware-In-The-Loop Testing System For Cubesat Components, Vahini N. Patel, Victoria Coverstone

Small Satellite Conference

Hardware-in-the-loop testing systems, commonly known as FlatSats, are testbed systems in which spacecraft subsystems, such as the onboard computer (OBC), power system, attitude determination and control system (ADCS), and communications, are laid flat and interconnected as they would be in an actual spacecraft. This arrangement gives easy access to each subsystem, enabling hardware and software testing and troubleshooting without risking fully assembled flight hardware.

FlatSats are widely used throughout the aerospace industry, from government agencies like ESA and NASA to private companies and university research labs, due to their versatility in enabling parallel development. This accelerates timelines and reduces …

Characterizing Rolling-Shutter Distortions In A 1u Cubesat Camera Using Led Strobe Imaging, Sharon Chan, Arseniy Dolgov, Andrea Schildhorn, Jenny Zhu, David Michelson

Small Satellite Conference

The ArduCAM OV5642 rolling shutter sensor was selected for ALEASAT because its simpler design results in reduced cost, power consumption, and heat generation. Although rolling shutter readout can introduce image skew due to the relative motion between the CubeSat and Earth, these sensors provide sufficient resolution and sensitivity within mission constraints. The feasibility of de-skewing, therefore, depends on the stability and predictability of the rolling shutter readout. Camera testing is not currently included in ISO 19683 (Space Systems – Design qualification and acceptance tests of small spacecraft and units). This work could be a step towards addressing that omission.

The …

Power Simulation Framework For Korucusat-2 Using Freeflyer, Sahil Singh, Annabel Rong, Mukund Karthikeyan

Small Satellite Conference

A FreeFlyer-based power simulation was developed for KORUCUSAT-2, a low Earth orbit CubeSat designed to monitor silicon-anode battery behavior in space. The spacecraft model uses body-mounted solar panels with five modules on each of the +X, -X, +Y, and -Y faces. The simulation integrates orbital propagation, Earth shadowing, Sun-incidence angle, ground-station visibility, mode-dependent subsystem loads, and battery-state propagation to estimate electrical margin. Battery watt-hours and normalized state of charge are updated at each 30 s step so that critical, low-power, operations, and transmission modes can be evaluated against stored-energy limits. The framework provides a traceable prelaunch test bench for power-system …

Design And Testing Of A Compact Hold-Down And Release System For A Formation Flying Micro Satellite; Seirios, Takahiro Takano, Yoshihisa Shimada, Takahiro Yamazaki, Masaki Ito, Itsuki Fujiwara, Satoshi Ikari, Shinichi Nakasuka

Small Satellite Conference

SEIRIOS(Space Experiment of IR Interferometric Observation Satellites)

• Demonstrates accurate formation flying (FF) technology with three microsatellites (two10 kg-class and one 60 kg-class)

Hold-Down and Release System (HDRS)

1. Retain the Deputy-Sats on the Chief -Sat during the launch.
2. Enable Interferometric observation in the docking configuration with no structural deformation.
3. Enable separation of the Deputy-Sats in orbit.
4. Avoid collision during separation

Launch Load Condition(Tentative)

The response amplification factor within the Chief-Sat was empirically set as below.

Herding Cubecats: Challenges And Lessons Learned From A Student-Led Cubesat Organization, Matthew Verbryke, Samuel Kohls, Nathan Nguyen, Michael Carovillano, Donghoon Kim

Small Satellite Conference

1. What is CubeCats?

CubeCats is a student-led technical engineering organization founded in 2015 at the University of Cincinnati (UC) with the mission of providing its members with hands-on, educational experience in space systems engineering, primarily through the design, development, testing, launch, and operation of flight-worthy CubeSats and High Altitude Balloons.

CubeCats’ operating model differs significantly from many university-based satellite programs:

• The organization is entirely managed and run by students, the majority of whom are undergraduates (UC faculty and staff serve primarily in an advisory role)
• The organization is entirely volunteer-based, with no direct integration into coursework or on-campus research …

Iterative Determination Of Pressures In The Refueling Process Of The Pw-Sat3 Satellite, Jakub Paziewski, Michał Niewiadomski, Paweł Senda, Jakub Dresler, Mikołaj Kmin, Kacper Kordek

Small Satellite Conference

PW-Sat3 is a 3U CubeSat being developed by the Students’ Space Association at the Warsaw University of Technology. It is a third satellite in the PW-Sat series, following PW-Sat with a deorbitation tail and PW-Sat2 with a deorbitation sail. PW Sat3 will be equipped with a warm-gas propulsion system and an authorial AOCS written by the students.

The final goal is to perform orbital decay by lowering the perigee. Secondary goals include taking pictures of the planet and evaluating innovative Earth horizon sensors using the satellite as a platform for amateur radio experiments.

Tracking Assembly For The Pulse-A Optical Ground Station, Rodrigo Spinola E Castro, Ashley Ashiku, Elizabeth Rosario, Juan Ignacio Prieto Asbun, Robert Pitu, Tian Zhong

Small Satellite Conference

PULSE-A is the University of Chicago’s student-led 3U CubeSat mission to demonstrate a space-to-ground optical downlink at a data rate of 1 to 10 Mbps using circular polarization shift keying (CPolSK).

Micro-Servicer Swarms For Responsive Smallsat Sustainment: The Sdaw Mothership Architecture, Wanjiku Chebet Kanjumba

Small Satellite Conference

The Challenge:

Sustaining The Mega-Constellation Era: LEO has shifted from a sparse domain into critical global infrastructure. With thousands of satellites on-orbit and tens of thousands more planned, sustainability is no longer guaranteed by launch activity alone; it depends on the ability to service, repair, and responsibly dispose of assets at scale.

• 7,500+ operational satellites in LEO (2024); 50,000+ projected within a decade
• 1,500+ trackable fragments from the 2021 Russian ASAT test; 1,700+ Starlink avoidance maneuvers followed
• ≥ 5 / yr large debris objects removed from LEO yearly to stabilize it (Liou & Johnson)

The Servicing Gap: MEV, OSAM-1, and …