Aerospace Engineering Commons^™

Progressing From High-Altitude Balloon Validation To Orbit: Establishing Cubesat Capability In Nevada Through Incremental Design, Kylee Brahma, Leandro Araiza, Christian Ługowski

Small Satellite Conference

UNLV ATLAS-1—Analysis of Temperature and Radiation in Low-Earth Orbit for Analog Studies—is a student-led 1U CubeSat mission at the University of Nevada, Las Vegas. The project uses an incremental approach, progressing from mock-satellite prototypes to high-altitude balloon flights and, ultimately, orbital deployment. By increasing system fidelity alongside student experience, UNLV ATLAS-1 aims to create a repeatable pathway for CubeSat development in Nevada and beyond.

Relative Position Determination For Satellite Formation Flying Using Radio-Wave Strength Considering Antenna Deformation, Sho Watanabe, Takaya Inamori, Yosuke Kawabata

Small Satellite Conference

Background:

Increasing use of formation flying in space missions:

• Requires formation establishment and maintenance
• Relative orbit determination is essential

Conventional Methods

• Camera
• Laser
• GNSS

Large size and mass are mostly required

Depends on the orbit and satellite attitude

Using received signal strength can overcome these limitations.

Thermal Analysis Of Small Satellites, Devansh Patel

Small Satellite Conference

Accurate thermal modeling is essential to spacecraft design, ensuring components remain within operational temperatures throughout orbit. This study develops and validates thermal models of increasing complexity to gain practical experience in spacecraft thermal analysis.

The GRIFEX mission is a 3U CubeSat launched in a 634 km circular polar orbit by the Michigan Exploration Laboratory (MXL). The CubeSat observed both 90° and 0° beta angle orbits during its mission, making it optimal for comparing thermal analysis results for small satellites in low Earth orbit.

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

Small Satellite Conference

• Magnetic field generation and compensation are essential for laboratory testing of an attitude determination and control system (ADCS) for small satellites. Since commercial magnetic test facilities are often unavailable or impractical for university laboratories, such setups are typically developed in-house. A controlled magnetic environment allows for reliable magnetometer characterization, magnetorquer testing, and evaluation of attitude control algorithms, enabling repeatable ADCS experiments under well-defined conditions.
• At our university, a CubeSat-class ADCS is being developed from the ground up by students, with a focus on hands on hardware development and experimental validation. The current ADCS prototype includes magnetic sensors, custom-developed magnetorquers, and …

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.

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.

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 …

Concept Of Operation Logic And Implementation Expectations For Multimode Propulsion Technology Demonstration Missions, Logan Thompson, Michael Harrigan, Theresa Sandborn, Victoria Coverstone, Joshua L. Rovey

Small Satellite Conference

Traditional single-mode propulsion systems are typically optimized for either high-thrust, short-duration maneuvers (chemical propulsion) or high-efficiency, low-thrust operations (electric propulsion). For CubeSats, which are limited by mass, volume, power, and system complexity, carrying separate propulsion systems for each mission phase is often impractical. Multimode propulsion systems overcome this limitation by combining chemical and electric propulsion within a shared architecture, allowing a single spacecraft to perform both rapid maneuvers and efficient long-duration orbit maintenance.

Demonstrating a multimode propulsion system requires more than operating two propulsion modes on the same spacecraft. Shared propellant, feed systems, thermal interactions, power usage, and transitions …

A Cubesat-Based Data Collection Architecture For The Catarina Constellation: Complementing Legacy Brazilian Data Collection System With Lora, Vitória Beatriz Bianchin, Carlos Augusto Porto Freitas, João Cláudio Elsen Barcellos, Gabriel Mariano Marcelino, Talita Sauter Possamai, Eduardo Augusto Bezerra

Small Satellite Conference

• The Catarina Constellation is a Brazilian CubeSat initiative created to enhance environmental monitoring and satellite-based environmental data collection across Brazil.
• The project was named after Hurricane Catarina (2004), the first recorded hurricane in the South Atlantic, which exposed the need for improved space-based monitoring of extreme weather events.
• The constellation aims to expand the Brazilian Satellite Data Collection System (SBCD) by evaluating new communication technologies, enabling a gradual modernization of the country’s environmental monitoring infrastructure.

Development Of A Compliant Mechanism Mechanical Battery For Satellite Applications, Trevor Carter, Bryce Christensen, Ryan Day, Anthony Bridge

Small Satellite Conference

Objective:

Traditional space power systems face severe limitations: chemical batteries decay in extreme thermal swings or drain over long dormant periods, and radioactive units lack the specific power needed for peak operational loads. BYU Rocketry’s Phoenix payload, a 3U CubeSat that competed in the 2026 SDL Payload Challenge addresses these gaps. Phoenix is a proof-of-concept mechanical battery that augments primary power systems, enabling peak-load operation and recovery from dormancy.

Development Of Low-Cost And Mobile University Ground Stations, Michael Cargill, Matthew Watson, Patrick Bailey, Jacob Boutin, Wout De Backer

Small Satellite Conference

Recent years have seen a deluge of university-class small satellite missions, driving an increase in demand for ground stations. SatNOGS is an open-source network of ground stations allowing users to schedule observations on each others’ hardware. Most stations are fixed in-place. Mobile stations lack endurance or are high cost. There is a gap for a low-cost option for groups needing mobility.

Investigation Of Functional Realization Of Optically Transparent Patch Antenna For Cubesat Downlink, Jaret Riggs, Ethan Wayland, Alivia Mckinlay, Isaiah Crookston, Samuel Green, Ernest Green, Tevis Hadley, Reyhan Baktur

Small Satellite Conference

The Get Away Special Radio and Antenna Transparency Satellite (GASRATS) is a 2U technology demonstration CubeSat. The spacecraft will demonstrate the feasibility of an optically transparent solar panel-integrated patch antenna in a spacecraft application. The solar panel integrated with meshed antenna efficiently uses external surface area, allowing for communications and power generation on a small CubeSat.

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 …

Project Minerva: High-Altitude Weather Balloon Cubesat Research Platform, Gannon English, Gabrielle Guirguis, Jose Murphy, Lena Wang, Ethan Yemm

Small Satellite Conference

Minerva is an undergraduate student-led high-altitude balloon (HAB) platform developed to provide repeatable, low-cost, and flight-proven testing of experimental payloads and communications systems in near-stratosphere environments. Originally an atmospheric data experiment, it has evolved into a modular testbed supporting missions for both internal research and external student organizations.

Minimum Variable Speed Control Moment Gyros (Vscmg) Cluster Sizing For Full Three-Axis Smallsat Attitude Control: A Numerical Study, Khang Nguyen, Christopher Damaren

Small Satellite Conference

Small satellites demand high-resolution imaging, optical inter-satellite links, precision science — demand agile, accurate attitude control under tight mass, volume, and power.

Momentum-exchange actuators are the standard propellant-free solution:

• Reaction wheels: precise, but low torque authority
• CMGs: high torque, but singularity-prone
• VSCMGs: variable wheel speed and gimbal angle → high torque, added DOFs for singularity avoidance, dual RW/CMG operation

The gap: VSCMG research has focused on 4-unit pyramid clusters, whose redundancy costs actuator count, volume, and power — resources SmallSats can least afford. The minimum cluster size for practical three-axis control is not well established.

Solar-Assisted Battery Charging For The Chipsat Architecture: Chipsat Updates And Validation For The Descent Mission, Mark Lohatepanont, Joshua Umansky-Castro, Val Zeitlin, Matthew Hurford, Mason Peck, Andrew Filo, Alex Burke

Small Satellite Conference

DeSCENT is a suborbital mission to deploy 100 ChipSats from Blue Origin's New Shepard near 100 km altitude. The experiment characterizes ChipSat free-fall kinematics and dispersion, and demonstrates their potential for distributed atmospheric sensing. The updated ChipSat combines rechargeable energy storage and body-mounted solar cells with GPS, sensing, onboard logging, and 915 MHz LoRa communications. Lab testing and high-altitude balloon flights validate integrated power operation and long-range communications performance. Preliminary mechanical testing supports the remaining deployment and flight-verification effort.

Tbearr: Tardigrade Bio-Exploration Reproduction Research Payload, Chloe Nissen, Jameson Feeley, Kylie Nager, Wilmar Galvez Alfonso, Amber Paul, Sean Crouse, Larry Fineberg, Francisco Crespo Cutillas

Small Satellite Conference

The mission aims to design and build an external ISS payload module investigating the reproductive response of Hypsibius exemplaris (tardigrades) to prolonged radiation in Low Earth Orbit. Experimental success will be measured by population density, as well as analysis of glutathione (GSH) and glutathione disulfide (GSSG, counterpart to GSH) via spectrophotometric assays. This will determine the amount of reactive oxygen species (compounds that cause cellular damage, ROS) generated, and how much of it was neutralized. In-orbit experimentation data, through post-mission experimentation, will be analyzed through on-board or astronaut post-processing and testing procedures. This will provide insight into the mechanisms behind …

The Effects Of Space On Pharmacology And Traditional Medicine: A Review Of Current Literature And Its Potential Impacts On Space Therapeutics, Pratyush Majumdar

Small Satellite Conference

Astronauts in space commonly take medicine for sleep disorders, muscle aches, and other miscellaneous conditions. These medications are taken under the assumption that they will work in space comparable to their effect on Earth, but mounting evidence is emerging to demonstrate that this is not the case. Using the principles of pharmacokinetics and pharmacodynamics, there are many physiological changes that alter how a drug is processed, changing their therapeutic effect. As mission times get longer, there is a heavier need to understand these changes and compensate for them in order to keep astronauts safe.

Lighting Up The Moon: A Scheduling Framework For Cislunar Space Based Solar Power Orchestration, Vaibhav Bhosale, Andrew Woo, Ada Gavrilovska, Christopher R. Valenta, Ketan Bhardwaj

Small Satellite Conference

Surviving the Lunar Night

• 14 Earth day lunar nights
• More batteries, more mass, higher cost