Digital Commons Network^™

Review Of Microgravity Biotechnology For Space Applications: The Anujiva Perspective, Saranya Ravva, Yukti Makkar, Abeneth Ramachandran, Sai Kiran Parre

Small Satellite Conference

Biomanufacturing in microgravity presents transformative opportunities for biotechnology beyond the limitations of terrestrial environments. Gravity-driven convection, sedimentation, and contamination risks often hinder biological productivity on Earth. In contrast, space-based conditions enhance protein crystallization, three-dimensional cell culture, and the production of novel biomaterials. This review synthesizes recent advancements in microgravity-enabled biotechnology, drawing from recent peer-reviewed literature and mission data.

We focus on the emerging field of autonomous bioreactor systems for space applications, emphasizing innovations in miniaturization, closed-loop environmental control, and real-time sensing. As a representative case study, we examine the AnuJIVA initiative, a CubeSat-based platform engineered for cultivating microorganisms such as …

High Resolution, Wide Swath Sar Observation From Disksat At Vleo, Hirobumi Saito, Yasuyuki Miyazaki, Michio Takikawa, Tien M. Nguyen, Roy Nakagawa, Ching-Yao (Tony) Chang, David Hinkley, Ryo Natsuaki, Mitsuteru Kaneoka, Jiro Hirokawa, Kazuyuki Nakamura

Small Satellite Conference

This paper proposes a novel concept of quasi-two-dimensional SAR (synthetic aperture radar) satellites, SAR DiskSats, featuring a deployable passive slot array antenna (De-PSAA) that can be compactly folded within the quasi-two-dimensional (Q-2D) satellite body. This Q-2D configuration allows for potential flexible solar cell sheets to be installed on the backside of the antenna, as the antennas do not dissipate heat. This satellite configuration is also suitable for stacking within a rocket fairing for the mega-constellation launch of SAR DiskSats into VLEO (very low Earth orbit). The proposed DiskSat's thin edge cross-section reduces aerodynamic drag, enabling the satellite to operate at …

Kentucky Re-Entry Probe Experiment-3: The Third Hypersonic Flight Of The Krups Capsules, Bruno Tacchi, Eric T. Adams, Alexander R. Barrera, Asa C. O'Neal, Aaron Cramer, James E. Lumpp, Savio J. Poovathingal, Alexandre Martin

Small Satellite Conference

The Kentucky Re-entry Universal Payload System (KRUPS) is a small flight capsule with dimensions of 11 by 8.5 inches and a sphere-cone geometry. KRUPS aims to serve as a cost-effective testbed for hypersonic atmospheric entry experiments, collecting thermal response and flight data during re-entry and testing novel thermal protection systems (TPS). The forebody of the capsule is fitted with an instrumented TPS containing thermocouples and pressure ports. Furthermore, the instrumentation suite contains a high-g accelerometer, a GPS, an IMU, and a spectrometer.

The KRUPS project started in 2013. Since then, the capsule has flown five sounding rocket missions, a high-altitude …

Astra – Autonomous Satellite Technology For Resilient Applications: A Technology Demonstrator, Lauren Underwood, Fernando Figueroa, Zachary Lewton, Landon Tynes, Travis Martin, Jonathan Morris, Quentin Oswald, John Curry

Small Satellite Conference

ASTRA is an on-orbit technology demonstrator establishing a new paradigm for implementing on-board “thinking.” ASTRA is a system-level autonomy capability (including digital twins, anomaly detection, diagnostics/prognostics, and mission management) enabled by an innovative technology, NPAS - NASA Platform for Autonomous Systems. NPAS is developed by NASA Stennis Space Center (SSC) Autonomous Systems Laboratory (ASL) with support from NASA Exploration Systems Development Mission Directorate (ESDMD) Advanced Exploration Systems and Mars Campaign Office. ASTRA leverages NPAS for on-board “thinking” autonomy. ASTRA also includes advanced hardware required for implementing autonomy. ASTRA Flight Software (FS) is running on commercial hardware that provides the computational …

On-Orbit Validation Of An Ai-Enabled Cloud Removal And Compression Solution For Eo Satellites, Rosana Rodríguez-Bobada, Jose Manuel Heredia-Oliver, Pablo Tomás Toledano González, Carlos Espinosa-Peral, José Luis Espinosa-Aranda, Tom Hendrix, Amaury Perrocheau, David Rijlaarsdam, Aubrey Dunne

Small Satellite Conference

Optical Earth Observation (EO) sensors can be significantly affected by atmospheric conditions, particularly cloud cover, which can obscure their images and reduce the information content in the final image. It is estimated that over 50% of the Earth’s surface is covered by clouds at any given moment. As a result, up to half of the data captured by visible EO satellite imagers is rendered unusable for most applications. Transmitting this unusable data, even in a compressed form, unnecessarily utilises valuable communications downlink bandwidth. This is particularly acute for hyperspectral EO missions, where the tens to hundreds of bands per acquisition …

The Shorthorn: May 15, 1956

The Shorthorn Newspaper Collection: 1950s

No abstract provided.

Slalom: A Mission Concept For Autonomous Very Low Lunar Orbit Operations, Jeffrey S. Parker, Bradley Cheetham, Charles Cain, Ethan Kayser

Small Satellite Conference

A Sustained Low-Altitude Lunar Orbital Mission (SLALOM) maintains an orbital path very close to the surface of the Moon: passing within 1–5 kilometers of topographical peaks and maintaining an average altitude under 10 kilometers. This extremely low orbit enables high-resolution observations of the Moon but requires a new class of autonomous navigation and stationkeeping. The au-tonomous software system, ALPINE (Auto-maneuver Location Processor using Integrated Navigation Estimates), fuses real-time optical navigation data with one-way and cross-link radiometric tracking data to maintain continuous and autonomous custody of the spacecraft. This paper examines a stationkeeping strategy that maximizes surface coverage of desirable locations …

Advancing Space Weather Research With The Next-Generation Space Weather Probes, Justin Wellington, Rowan Antonuccio, Kade Howes, Benjamin Lewis, Todd Wilson, Charles Swenson

Small Satellite Conference

Accurate characterization of ionospheric conditions is essential for improving space weather forecasting and mitigating its impacts on communication, navigation, and space-based systems. Utah State University’s Center for Space Engineering has developed the second-generation Space Weather Probes (SWP2) instrumentation suite, optimized for deployment on small satellite platforms. Building upon experience from the Scintillation Prediction Observations Research Task (SPORT) mission, SWP2 integrates advanced Langmuir probes, floating potential double probes, and an RF impedance probe onto a compact, FPGA-controlled electronics module, conforming to the standard 9×9 cm CubeSat form factor. The design provides complementary diagnostic measurements of electron density, electron temperature, electric fields, …

Chipsat Design For The Descent Mission, Matt Hurford, Bryan Peters, Joshua Umansky-Castro, Corbin Heywood, Andy Filo, Alex Burke

Small Satellite Conference

The Demonstration of Suborbital ChipSats Ejected from New Shepard Test Flight (DeSCENT) mission, conducted by Cornell’s Space Systems Design Studio (SSDS) in partnership with the Applied Physics Laboratory (APL), is a suborbital endeavor that aims to deploy 100 ChipSats from a Blue Origin New Shepard rocket when the rocket reaches 100 km above the Earth’s surface. ChipSats are a type of FemtoSat (satellite with a mass less than 100 grams) that can fit into the palm of your hand and contain all the fundamental functionality of a spacecraft. The mission’s primary objective is to refine models that predict the freefall …

Productization And Qualification Of A 22n Bipropellant Hydrogen Peroxide Engine, Thomas White, Vivek Vidyarthi, Avery Clotfelter

Small Satellite Conference

As the space industry expands quickly and green propellants enjoy growing interest, the key question of research is no longer basic viability but productization. The most valuable engine is one that is qualified and available as close to “off the shelf” as possible. But publications on the process of taking an engine from first demonstrations to true product status are rare. This paper describes the process of transitioning Benchmark Space System’s 22N Ocelot engine – first flown as the 1.0 product version in 2022 – into a high-volume, well-characterized product, including details on the qualification program for the 1.2 version, …

Leopard: Demonstrating Cubesat Technologies For Light Scattering Observations And Satellite Positioning In Leo For Future University-Based Lunar Missions, Necmi Cihan Orger, Victor Hugo Schulz, Jose Rodrigo Corodova-Alarcon, Hanadi Abdalla, Mehmet Esit, Makiko Kishimoto, Sara Aziz, Mengu Cho, Minh Pham Anh, Hery Steven Mindaro, Subsinchai Ratatamanun, Enkhmend Ochirsukh, Husseinat Etti-Balogun, Kubo Shota, Jeje Kudakwashe, Thibaut Tena, Rafiki Yves Ndayishimiye, Daisuke Nakayama, Alper Sanli, Konosuke Nishinaga, Akihiro Oboshi, Edgar Mujuni, Ramson Munyaradgi Nyamakondiwa, Im Polimey, Hiroto Hidaka, Hirokazu Masui, Josue Reynel Galindo Rosales

Small Satellite Conference

The LEOPARD (Light intensity Experiment with On-orbit Positioning and satellite Ranging Demonstration) satellite is a 3-unit (3U) CubeSat platform to demonstrate several technologies and payloads in low Earth orbit (LEO) prior to future lunar CubeSat missions. After deployment from the International Space Station (ISS), it plans to perform the following missions, including onboard processing of Earth-origin one-way radio ranging signals (OPERA), multispectral imaging to monitor light scattering above the horizon (MSC), single event latch-up detection (SEL), solar panel deployment using shape memory alloy (SMA), and ambient magnetic field measurements. First, the OPERA mission will validate critical steps towards deep-space positioning …

Moral And Ethical Nature In Confucian Liang-Zhi And Islamic Fitra: Comparative Perspectives On Innate Morality, Yanrong Shi

Comparative Philosophy

This article offers a comparative philosophical analysis of Confucian liang-zhi (innate moral knowledge) and Islamic fitra(primordial nature), focusing on their accounts of innate morality and moral epistemology. Drawing on classical Confucian sources—especially the praxis-oriented interpretation of Wang Yangming—and foundational Islamic texts and commentary, the study demonstrates that both traditions posit an inborn moral faculty grounding ethical universality and responsibility. Wang Yangming’s liang-zhi is conceived as an innate moral principle that, under the imperative of zhi (to actualize or extend), is continually activated through moral practice. In parallel, fitra is understood as a God-given orientation to truth, cultivated and safeguarded through …

How Theravāda Buddhism Enriches The Language Of Thought Hypothesis: Beyond Syntax, Juanjuan Cheng, Sumanasara Sandamadulle

Comparative Philosophy

The Language of Thought Hypothesis (LOTH) posits that mental states operate through a language-like representational system physically implemented in the brain. However, this purely symbolic approach faces a significant limitation: certain mental phenomena—such as intuitions, emotions, and intentions—lack the syntactically compositional structure required by LOTH and therefore cannot be adequately explained within its symbolic framework. To address this theoretical challenge, we turn to Theravāda Buddhism (TB), an early Buddhist tradition that integrates rigorous philosophical inquiry with meditative practice. Remarkably, TB began to prefigure a solution to LOTH’s limitations over 2,300 years ago. Although LOTH and TB differ …

High-Performance Green Hydrazine-Based Propellant For Small Spacecraft, Robert K. Masse, Andrew R. Haviland, Benjamin A. Glassy, Ronald A. Spores, Joshua L. Rovey

Small Satellite Conference

Whereas the last decade has seen a notable expansion in the number of small spacecraft on orbit, a lack of high-total-impulse chemical propulsion options continues to hamper their complete proliferation into mission arenas requiring dynamic maneuvering. This has been particularly true at the NanoSat/CubeSat scale, where volume limitations are most constraining. Because SmallSats are generally launched as secondary payloads, green ionic liquid propellants such as ASCENT and LMP-103S have been recognized as particularly advantageous in that they introduce minimal logistical impacts to primary payload integration workflow. However, despite the substantial packaging advantages conferred by their high impulse density, these propellants …

In 8 Years From Design To Launch: Objectives, Challenges And Risk Mitigation Of The Educational Student Cubesat Project Source, Philipp Hoffmann, Kaja Gebhard, Mario Spahr, Klemens Boltenhagen, Michael O'Donohue, Daniel Galla, Robin Schweigert, Natascha Bonidis, Sabine Klinkner

Small Satellite Conference

The Stuttgart Operated University Research CubeSat for Evaluation and Education (SOURCE) project is a 3U+ CubeSat developed in collaboration between the Small Satellite Student Society at the University of Stuttgart (KSat e.V.) and the University of Stuttgart’s Institute of Space Systems. This educational satellite mission is designed to provide students with hands-on experience in all phases of satellite development, from the initial concept to the final mission operations. SOURCE’s development began in 2018 and has been supported by ESA’s Fly Your Satellite! program since 2020. Over the past seven years, more than 500 students have had the opportunity to work …

Game-Changing Technologies For Green Propulsion Operating With 98% Hydrogen Peroxide, Pawel Surmacz, Adrian Parzybut, Michal Ranachowski, Zbigniew Gut, Michal Alaszkiewicz

Small Satellite Conference

The propellant grade hydrogen peroxide is coming back to space industry. While launcher applications would accept lower grades of High Test Peroxide (HTP) for cost reduction, the highest possible concentration matters much more for in-space propulsion. Every 1% in peroxide concentration translates to the propulsive performance (specific impulse) roughly in 1% for monopropellant and 0.5% for bipropellant.

The highest HTP grade provides certain advantages. While being more reactive, it requires less catalyst for its full decomposition, resulting in hardware mass and cost reduction. When used with any kind of bipropellant (either catalyst-augmented or hypergolic, and including hybrid), the highest grade …

Target Selection For The Pandora Smallsat: A Nasa Mission To Disentangle Stellar And Exoplanet Atmosphere Signals, Knicole Colón, Elisa Quintana, Thomas Barclay, Benjamin Hord, Jessie Dotson, Daniel Apai, Benjamin Rackham, Jason Rowe

Small Satellite Conference

The Pandora SmallSat mission was selected for implementation in 2021 as part of NASA’s Astrophysics Pioneers Program. Pandora is designed to monitor stellar variability while studying the atmospheres of transiting exoplanets via transmission spectroscopy. The transmission spectroscopy technique is one of the best methods to identify the makeup of exoplanetary atmospheres now and in the coming decade. However, stellar variations that occur from the presence of, for example, cool star spots, have been shown to contaminate the exoplanet atmosphere spectra obtained with high-precision transmission spectroscopy measurements. This stellar contamination leads to ambiguous interpretations when attempting to distinguish features like potential …

Performance Evaluation Of 1 U+ Module Of Water Ion Thruster With 7000 Ns Of Total Impulse, Yuichi Nakagawa, Hiroto Saito, Jun Asakawa

Small Satellite Conference

Water has emerged as a promising propellant for small satellite propulsion systems due to its inherent advantages in safety, affordability, and ease of handling. Traditional chemical propellants such as hydrazine pose significant safety risks due to their toxicity and explosiveness, while electric propulsion systems often rely on high-pressure gases like xenon and krypton, which present logistical and supply chain challenges. Although water exhibits lower propulsive performance, particularly in terms of specific impulse, its practical benefits have gained attention with the rise of CubeSats and nanosatellites, where mission requirements prioritize simplicity and safety over maximum efficiency. Various water-based propulsion technologies have …

Rhok-Sat: Investigating Perovskite Solar Cell Performance And Degradation In Low Earth Orbit Through A 1u Cubesat, José R. Pastrana, Anas Matar, Kerry Tang, Damian Nguyen, Marouf M. Paul, Mallory Miller, Phuc H. Nguyen, Jasper Scherz, Zheng Yu Wong, Jess G. Hamer, Olivia A. Kaufmann, Benjamin T. Wilson, B. Burnham

Small Satellite Conference

RHOK-SAT is a 1U CubeSat scheduled to launch in September 2025 aboard a resupply mission to the International Space Station (ISS) through NASA’s CubeSat Launch Initiative (CSLI) program. Its mission is to characterize the performance and degradation of six experimental perovskite solar cells in low Earth orbit for 12 months. Characterization consists of current-voltage measurement taken by one dedicated microcontroller per solar cell. Measurements are performed when the cells are in direct sunlight, determined via a quadrant photodiode. A silver-alloyed copper indium gallium selenide (ACIGS) solar cell serves as a reference for comparative analysis due to its well-characterized behavior. Each …

Extended Testing Of A Steam-Powered Propulsion System For Rapid-Orbit Corrections: A Viable Alternative To Chemical Propulsion, Marco Pavan, Ivan Timofeev, Vladimir Fedorov, Jinyoung Shin

Small Satellite Conference

The Steam Thruster One is an electro-thermal propulsion system capable of delivering a thrust level up to 20 mN, using 20 W of power and reaching a total impulse of about 1200 Ns in its 2U configuration. The system operates solely on low-pressure water, ensuring complete safety for integration and operations both on the ground and in space. The propulsion cycle involves converting liquid water into superheated steam, which is then expanded through a nozzle to generate thrust.

The propulsion system was tested in space in Q3 2023 and Q2 2024, where it successfully demonstrated short propulsion manoeuvres. However, for …

Stp-H12-Vantage: Combining Visual And Event-Based Sensing For Earth Observation, Diego Wildenstein, Michael J. Cannizzaro, Ian Peitzsch, Linus Silbernagel, Joshua Poravanthattil, Peter Drum, Mark Hofmeister, Cole Bowman, Natan Herzog, Evan W. Gretok, Alan D. George

Small Satellite Conference

Conducting Earth-observation tasks from orbit can provide valuable research insights in fields such as meteorology, geology, forestry, cartography, and defense. Developing and building space payloads for Earth observation poses significant challenges, including the high cost of radiation-tolerant systems, the widening gap between current state-of-the-art apps and the capabilities of space-grade processors, and the increase in fidelity of modern sensors. Many Earth-observation missions typically collect data by leveraging visual and/or multispectral imagers. However, when using conventional imaging, there can be significant losses in context due to the frame-based operation of these sensors, as well as both relevant and irrelevant data mixed …

An Exploratory Study Of Soft Skills Development Expectations In Two-Year Generation Z College Students, Kelli Hallsten Erickson

The Interactive Journal of Global Leadership and Learning

Workplace demands around competent demonstration of soft skills have been steadily increasing; therefore, institutions of higher education have started focusing attention on instilling these skills within their student populations. The latest generational cohort to enter college and the workforce, Generation Z, has only recently begun to be studied for the impact of its members’ attitudes towards work and how those might change employer expectations around soft skills. A research gap exists, however, regarding students in Generation Z attending two-year schools and which soft skills they feel are most valuable to their future careers. This study sought to explore those attitudes …

Microgravity Testing Of A Thermal Start Basket For Propellant Repositioning, Hugh Chen, Álvaro Romero-Calvo

Small Satellite Conference

CubeSat cold-gas propulsion increasingly relies on two-phase propellants stored in conformal tanks. However, state-of-the-art propellant management strategies for these systems result in significant portions of the tank being occupied by vapor, reducing the amount of storable propellant. They also require high power input for vapor expulsion, increasing mission complexity and limiting operational lifetime. These challenges highlight the need for a more robust propellant management approach. The VAporization for PrOpellant Repositioning (VAPOR) experiment investigates the feasibility of repositioning an ullage gas bubble of R-236fa using thermally-induced phase change in various propellant management devices (PMD). These devices utilize a heat source to …

Development Of The Music Hall Thruster Family For Small Satellite Missions: Current Status And Upcoming Missions, George-Cristian Potrivitu, Matteo Laterza, Khoo Kai Sheng, Nunki Pontianus, Suryono Gunawan Ali, Justin Ong, Dylan Lim, Zhuo Xuan Chua, Wei Jian Joshua Lim, Willem Frederik Von Lynden, Garreth Christopher Anwar, Mooi Meng Wai, Jian Wei Mark Lim

Small Satellite Conference

The MUSIC – MUlti-Stage Ignition Compact – Hall thruster family is developed to operate at system power below 100 W making it ideal for small satellites ranging from 3 U to a few 100 kg. The concept relies on the versatility of the MUSIC thruster unit which can be operated in various modes, and the modularity of the peripherals, i.e., the power and electronic control units, and propellant management assembly. This contribution expands the existing scarce literature on low-power Hall thruster systems that are qualified for flight, presents an overview of the capabilities of the MUSIC Hall thruster, past and …

Ecaps High-Performance Green Propulsion – Enabling Tactically Responsive Space Missions, Wilhelm Dingertz, Peter Thormählen, Odysseas Christofi

Small Satellite Conference

In a rapidly evolving geopolitical landscape where space is increasingly viewed as the fourth operational domain, tactically responsive launch capabilities and in-orbit maneuverability are critical. The ability to pre-load spacecraft and maintain them in a ready-to-launch state enables quicker response times, essential for strategic operations. Longterm storable, non/low-hazardous "green" propellants, such as ECAPS’ LMP-103S based on Ammonium DiNitramide (ADN), are key to this agility. These propellants offer improved performance, reduced environmental and operational risks, and facilitate faster spacecraft processing and storage. ECAPS High-Performance Green Propulsion (HPGP) technology has achieved extensive flight heritage with its 1N thruster, across 30+ missions, typically …

Consolidated Simultaneous Ranging And Clock Synchronization With Application To Positioning In Cis-Lunar Space, Junichiro Kawagichi, Shingo Nishimoto

Small Satellite Conference

The AOWR scheme functions as a set of transceivers connecting two entities: the ground station and the spacecraft. The phase difference information obtained from both sides intrinsically contains data related not only to the range but also to the clock difference simultaneously. The AOWR scheme can synchronize the clock onboard the spacecraft regardless of the distance. In cis-lunar space due to poor geometric configurations, until the position is determined, the clock difference cannot be established. It drastically improves and reduces the dilution-of-precision index. The paper will present the outcomes confirmed through demonstration experiments utilizing hybrid devices related to the GNSS …

Standards And Schematics For Intelligent Extensible Mission Architectures In Space, Evana Gizzi, Alan Gibson, James Marshall, Shannon Bull, Timothy Chase Jr., Jonathan Davis, Matthew Dosberg, Michael Johnson, Peter Knudtson, John Lucas, Michael Monaghan, Chris Robberts, Daniel Rogers, Bethany Theiling, Julie Breed, Larry Kepko, Carrie Vuyovich, Connor Firth, Lily Clough, Aaron Woodard, Brian Kempa, Caleb Adams, Robin Onsay, Sam Pedrotty, James Berck

Small Satellite Conference

As the space sector trends toward complex mission types, the demand for multi-asset, multi-generational, and multi-organizational paradigms has grown. It is critical that the spaceflight community builds the infrastructure needed to realize these mission architecture goals. To this end, we present a standard and schematic for intelligent extensible mission architectures, which will allow missions of the future to be distributed, heterogeneous, incremental, and interoperable for enhanced flexibility, adaptability, and responsiveness in space. We begin by describing a motivation for intelligent extensibility, followed by a review of related work in standards and autonomous multi-agent systems. Next, we present the theoretical definition …

Quarcs Light: Validation Of An Abbreviated Assessment Of Undergraduate Numeracy And Mathematics Affect, Isaac S. Rosenthal, Kate Follette, Vonna L. Hemmler, Catherine Sarosi, Sanlyn Buxner, Erin Galyen, Margaret Shea, Soon-Young Shimizu, Brendan Seto

Numeracy

In this study, we present evidence for the validity of a shortened form of the Quantitative Reasoning for College Science (QuaRCS) Assessment, a validated instrument assessing the numeracy and math-related affect of undergraduate students in general education/introductory science courses. Previously published analyses of QuaRCS data revealed that 1) roughly 30% of students found the assessment boring, leading to lower self-reported effort and 2) affective factors (e.g. numerical self-efficacy) were significant predictors of QuaRCS score. As a result, we reduced the length of the assessment from 25 to 15 quantitative items, and expanded the affective variable selection from three to eight …

Building Oklahoma’S First Cubesat Program: A Student’S Perspective, John O'Hara, Imraan Faruque, Peter Lopresti, Cannon Kilcrease

Small Satellite Conference

OKSat is a student-led, multi-university effort to launch Oklahoma’s first CubeSat. Built from the ground up, the program has provided students with hands-on experience in space systems engineering, leadership, and cross-institutional collaboration. This poster shares lessons learned from establishing and growing the program, highlighting strategies that support sustainable, student-driven satellite development—especially in regions without established aerospace programs.

Revolutionizing Space Thermal Control: The Breakthroughs And Applications Of Pulsating Heat Pipes, Matt Schultz, Jimmy Hughes, Mckenzie Sandberg

Small Satellite Conference

The development of Pulsating Heat Pipes (PHP) offers significant advancements in thermal control technologies. This poster reviews the fundamental mechanisms of PHPs, manufacturing processes, and focuses on how PHPs fit into the current thermal architecture for satellite, payload, and instrument thermal control to identify the best use cases and application of the emerging technology.