Digital Commons Network^™

Time-Evolved Constant Voltage Conductivity Measurements Of Common Spaceborne Polymeric Materials, Brian Wood, David King, Jr Dennison

Journal Articles

Long-duration current measurements were made for low-density polyethylene (LDPE), polyimide (PI), polyether ether ketone (PEEK), and biaxially oriented polypropylene (BOPP) to determine their bulk conductivity near room temperature as a function of time. These common thin-film spacecraft material samples were vacuum baked to remove moisture and volatile contaminants to better simulate space conditions. The constant voltage conductivity (CVC) method used a very stable, low-noise dc voltage source and measured the resulting current in a parallel plate geometry. Due to the extremely low conductivity of these four polymeric materials, extended experiments of up to ten days were necessary to establish equilibrium …

Career: Algebra And Representation Theory For Non-Semisimple Topological Field Theory, Matthew Young

Funded Research Records

No abstract provided.

Passive Precision Alignment For Thin-Panel Deployable Space Systems, Jake Sutton, Trevor Carter, Brooklyn Olson, David Wing, Fisk Lungreen, Larry Howell, Nathan Usevitch, Spencer Magleby, Mark Stephen

Small Satellite Conference

Optical satellite performance improves with increased surface area, which enhances light capture and sensor input. Deployable mechanisms allow satellites to remain compact during launch and expand in orbit but the large relative motion during deployment makes it difficult to achieve precision alignment in the final deployed state. This study focuses on designing passive hinges in rigid-panel origami-based deployable satellites for optical applications. A novel kinematic coupling method is developed, incorporating magnets, compact Lamina Emergent Torsional (LET) joints, and principles from Maxwell couplings. This system autonomously achieves alignment without motorized actuation. The design process involved iterative testing of ten two-panel hinge …

A Ka Band High Data Rate Transmitter For Leo Satellites Design And System Simulation, Jean-Hervé Corre, Ronan Foubert, Thomas Dehaene, Hugo Hartmann, Yann Prigent, Bertrand Lechevalier

Small Satellite Conference

This paper addresses the design of a high-throughput Ka-band transmitter for LEO satellites. This article particularly focuses on RF and microwave subsystems and system simulation.

The purpose of this transmitter (named KaLLISTO) is to operate the downlink from a LEO satellite to a ground station. High data rates are required to meet the expressed demand from satellite operators to enable much more data volume downlink. The equipment is the latest state-of-the-art qualified COTS based design. This design is perfectly adapted to New-Space programs, where cost effectiveness, performance and reliability are key factors. The allocated band goes from 25.5 to 27GHz …

Stari: Starlight Acquisition And Reflection Toward Interferometry, John D. Monnier, James Cutler, Michael Meyer, Caden Burkhardt, Akshat Dubey, Jacob Klingler, Raven St. Clair, Shivani Sunil, Daniil Voloshin, Leonid Pogorelyuk, Melissa Flores, Albert Ostoja-Starzewski, Simone D'Amico, Ethan Foss, Prachet Jain, Antonio Rizza, E. Glenn Lightsey, Althea Noonan, Kerri Cahoy, Gautam Vasisht

Small Satellite Conference

We introduce the NASA-funded mission STARI (STarlight Acquisition and Reflection toward Interferometry). We plan to demonstrate the first transfer of starlight between two separate spacecraft, a key technology step towards long-baseline interferometry. Consisting of two propulsive 6U CubeSats flying in Low Earth Orbit separated by ∼100 meters, STARI will reflect a small beam of starlight from the Chief spacecraft toward the Deputy spacecraft, where the light will be collected by an off-axis parabola and focused into a single-mode fiber. With the use of differential Global Positioning System (GPS), visual LED beacons and fast-steering-mirrors (FSMs), we aim for continuous high-throughput fiber …

Spacecraft-Initiated Scheduling Of Ground Stations: On-Orbit Results From Techedsat-11, Adam Gannon, Timothy Recker, Lucas Shalkhauser, Rachel Dudukovich, Janette Briones, Alejandro Salas, Malachi Mooney-Rivkin, Marcus Murbach

Small Satellite Conference

The commonplace practice of manually scheduling communications is challenged by complex and often unpredictable data needs of modern spacecraft. Automation has clear benefits to improve timeliness and efficiency of space communications. In this work we describe and experimentally demonstrate a suite of software which automates the process of scheduling contacts for satellite communications. Service is scheduled based on a spacecraft’s needs and contacts execute automatically without a human in the loop. Requests for service originate onboard the spacecraft, traverse a low-rate control channel to reach a terrestrial server, and are fulfilled by ground station assets. This work describes an experiment …

Optical Inter-Satellite Link Demonstration On Cubesats - Update On The Cubeisl-Iod Mission, Benjamin Rödiger, Jorge Rosano Nonay, Arvind Kumar Balan, Alberto Rodríguez Pérez-Silva, José Franciso Briz Valero, Cristóbal Nieto Peroy

Small Satellite Conference

Free-space optical communication has become a mature technology to extend and replace classical radio channels for data transmission from satellites to the Earth. The advantages of high data throughputs, resilience against electromagnetic disturbances and its robustness against jamming spoofing and eavesdropping makes laser communication attractive for governmental, defense authorities and commercial users. To enable global connectivity and interoperability beyond the line of sight, inter-satellite links are required and therefore terminals with high data rates are necessary to avoid communication bottlenecks. Size weight and power limitations on spacecraft demand highly efficient and miniaturized payloads, especially for use cases on smallest satellites. …

Deployable Diffractive Optical Elements For Small Satellite Lidar Missions, Adam Bahlous-Boldi, Leila Freitag, Amber Cooper, Mary Dahl, Afreen Siddiqi, John Leckey, Kerri Cahoy

Small Satellite Conference

SPECIES (Smart Polyimide Expandable Collector to enable Investigations for Earth Science) is a NASA Earth Science Technology Office (ESTO) project that explores the use of a deployable diffractive optical element (DOE) in a space-based lidar instrument for a 12–24U CubeSat operating in low Earth orbit (LEO). The DOE, a 0.6-meter hybrid multi-level Fresnel zone plate, is made using a tessellation of hexagonal molds, each with a unique number of diffractive levels. It is stowed for launch and deployed on orbit using a 3 meter long extendible boom, which positions the optic at the correct distance from the spacecraft, while guy …

Pulse-A Mission Overview: Optical Communications For Undergraduate Students, Logan Hanssler, Seth Knights, Graydon Schulze-Kalt, Juan Ignacio Prieto Asbun, Robert Pitu, Lauren Ayala, Rohan Gupta, Vincent Redwine, Spencer Shelton, Catherine Todd, Maya Mcdaniel, Sofia Mansilla, John Baird, Mason Mccormack, Leah Vashevko, Tian Zhong, Michael Lembeck

Small Satellite Conference

Recent advances in the size, weight, and power (SWaP) requirements for space-based sensing have dramatically increased the demand for high-bandwidth downlink. However, high data rate RF transceivers still pose significant SWaP and cost restrictions, especially for university-class CubeSat missions. Optical communication may provide a solution to this challenge, enabling data transmission with order-of-magnitude rate increases over RF while being both secure and SWaP-efficient. The Polarization-modUlated Laser Satellite Experiment (PULSE-A) is a University of Chicago mission to demonstrate optical downlink at a data rate of up to 10 Mbps using circular polarization shift keying (CPolSK). PULSE-A comprises a < 1.5U Optical Transmission Terminal, 3U CubeSat Bus, Optical Ground Station (OGS) employing an amateur telescope, and RF Ground Station (RFGS), all of which are being designed and integrated by a team of over 60 undergraduate students. The mission objective is threefold: (1) to provide hands-on educational experiences for undergraduate students, (2) to make hardware for optical communication systems more accessible via open-source design, and (3) to explore the viability and potential advantages of using CPolSK for optical downlink.

PULSE-A serves an …

Pulse-A Mission Overview: Optical Communications For Undergraduate Students, Logan Hanssler, Seth Knights, Graydon Schulze-Kalt, Juan Ignacio Prieto Asbun, Robert Pitu, Lauren Ayala, Rohan Gupta, Vincent Redwine, Spencer Shelton, Catherine Todd, Maya Mcdaniel, Sofia Mansilla, John Baird, Mason Mccormack, Leah Vashevko, Tian Zhong, Michael Lembeck

Small Satellite Conference

Recent advances in the size, weight, and power (SWaP) requirements for space-based sensing have dramatically increased the demand for high-bandwidth downlink. However, high data rate RF transceivers still pose significant SWaP and cost restrictions, especially for university-class CubeSat missions. Optical communication may provide a solution to this challenge, enabling data transmission with order-of-magnitude rate increases over RF while being both secure and SWaP-efficient. The Polarization-modUlated Laser Satellite Experiment (PULSE-A) is a University of Chicago mission to demonstrate optical downlink at a data rate of up to 10 Mbps using circular polarization shift keying (CPolSK). PULSE-A comprises a <1.5U Optical Transmission Terminal, 3U CubeSat Bus, Optical Ground Station (OGS) employing an amateur telescope, and RF Ground Station (RFGS), all of which are being designed and integrated by a team of over 60 undergraduate students. The mission objective is threefold: (1) to provide hands-on educational experiences for undergraduate students, (2) to make hardware for optical communication systems more accessible via open-source design, and (3) to explore the viability and potential advantages of using CPolSK for optical downlink.

PULSE-A serves an …

A Proposed Process To Define And Collect Project Information For Cost Estimation Of Cubesat Platforms, Ana Carolina Di Iorio Jeronymo, Lidia Hissae Shibuya Sato, Renan Guilherme Soares Menezes, Felipe Oliveira Tavares, Maria Eduarda Mora Camino-Priante, Luís Eduardo Vergueiro Loures Da Costa

Small Satellite Conference

Cost estimation is a key element in the planning and execution of CubeSat mission, as it helps ensure that resources are used efficiently and that mission objectives remain aligned with technical and operational constraints. A solid technical baseline - one that clearly describes the system’s characteristics - is essential for developing reliable cost estimates and for establishing a shared understanding of the project among stakeholders. This paper presents the cost estimation process used at the ITA Space Center for CubeSat platforms. The method follows a structured, eight-step approach adapted from NASA and ESA standards. The steps begin with receiving the …

A Proposed Process To Define And Collect Project Information For Cost Estimation Of Cubesat Platforms, Ana Carolina Di Iorio Jeronymo, Lidia Hissae Shibuya Sato, Renan Guilherme Soares Menezes, Felipe Oliveira Tavares, Maria Eduarda Mora Camino-Priante, Luís Eduardo Vergueiro Loures Da Costa

Small Satellite Conference

Cost estimation is a key element in the planning and execution of CubeSat mission, as it helps ensure that resources are used efficiently and that mission objectives remain aligned with technical and operational constraints. A solid technical baseline - one that clearly describes the system’s characteristics - is essential for developing reliable cost estimates and for establishing a shared understanding of the project among stakeholders. This paper presents the cost estimation process used at the ITA Space Center for CubeSat platforms. The method follows a structured, eight-step approach adapted from NASA and ESA standards. The steps begin with receiving the …

Launch Support: Managing Complementor Bottlenecks In The Disruptive Innovation Of Small Satellites, Yue Song, Yue Maggie Zhou

Small Satellite Conference

Small satellites represent a disruptive innovation that significantly reduces the time and cost of satellite production and launch. Despite the large number of small satellites launched today, initially, they were viewed as “second-class launch citizens,” with incumbent large-rocket companies resisting launching them. This paper examines how small-satellite manufacturers overcame this resistance before establishing their dedicated small-satellite ecosystem. We identify the adjustment costs that caused resistance from large-rocket companies and examine two specific strategies implemented by disruptors—technological standardization and forward integration—to mitigate these costs and gain support from large-rocket companies.

Novel Solutions For Cubecat Attitude Determination And Control Systems Using Pcb Magnetorquers And Low Power Control Solutions, Weston Willardson, Eero Ward, Harrison Thomas, Michael Evans, Michael Williams, Sarahi Oretga-Duran, W. Seth Nelson, David Long

Small Satellite Conference

Satellite attitude determination and control systems (ADCS) can be large, heavy, and expensive relative to a CubeSat’s size, weight, and cost requirements. We have developed a compact, low-mass, inexpensive ADCS prototype suitable for a student-class 1U CubeSat. We utilize three enabling technologies to reduce size, weight, and power (SWaP): 3-axis low-profile printed circuit board (PCB) magnetorquers, a basic sensor package, and computationally efficient control. The PCB magnetorquers are mounted on the exterior of the CubeSat frame to conserve internal volume for spacecraft electronics and payload. Attitude is determined by infrared horizon sensors and a magnetometer. The control algorithms utilize computer …

Deploying Post Quantum Cryptography On Newspace Satellites, Erik Lewerenz

Small Satellite Conference

We describe and implement a new key exchange protocol combining both Post Quantum Cryptography (PQC) and Elliptic Curve Cryptography (ECC). The protocol is designed to allow for authenticated key exchanges with a single satellite. The Triple Key Encapsulation Mechanism (KEM) protocol is designed to be secure against both classical and quantum attackers and retains its full security even if one of the two cryptographic schemes is broken. The protocol was implemented on two generations of Berlin Space Technology (BST) On Board Computers (OBC) and tested on the AFR small satellite in low earth orbit using an In Orbit Demonstrator (IOD) …

Development Of A Tool For Planning Fuel-Optimized Collision Avoidance Maneuvers, Saksham Jain

Small Satellite Conference

The need for collision avoidance maneuvers is expected to rise due to growing congestion in low-Earth orbit. This paper presents the development of a tool to automate the generation of collision avoidance maneuvers in response to conjunction events. The tool presented has allowed the Space Flight Laboratory (SFL) to eliminate concerns associated with human error, while concurrently addressing the expected increase in the need for these maneuvers without needing to impose any additional burden on flight dynamics engineers. The automation of this task has reduced the hands-on time required by over 80% when compared to the pre-existing workflow.

If the …

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

Small Satellite Conference

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

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

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

Small Satellite Conference

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

Next-Generation Earth Observation: Agile Satellites With Cmg Cluster For Enhanced Coverage, Andrea Coco, Simon Debois

Small Satellite Conference

The rapid growth of Earth observation demands cost-effective strategies, such as integrating COTS components and accelerating deployment. A key factor in mission efficiency is spacecraft agility, which enables faster reorientation, improved target tracking, and optimized data collection. A game-changing advancement is the revival of Control Moment Gyroscopes (CMGs) as cost-effective, high-performance actuators. Once constrained by high costs, recent manufacturing innovations and new providers have made CMGs more accessible. With superior torque efficiency and capability, CMGs greatly enhance agility, enabling faster reorientation and improved data collection compared to conventional reaction wheels. This paper presents a comparative case study demonstrating the advantages …

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

Small Satellite Conference

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

From Dishes To Distributed Arrays: Towards Efficient And Interference-Free Satellite Ground Stations, Rohith Reddy Vennam, Luke Wilson, Sesha Sai Rakesh Jonnavithula, Ish Kumar Jain, Dinesh Bharadia

Small Satellite Conference

The rapid growth of low Earth orbit (LEO) satellite constellations, driven by initiatives such as Starlink and Kuiper, has enabled global internet access, Earth observation, and emerging direct-to-device (D2D) applications. However, this surge in satellite deployments has outpaced the expansion of ground station infrastructure, creating a critical bottleneck for scalable and low-latency communication. Traditional ground stations, predominantly based on mechanically steered parabolic dishes, are ill-suited for tracking multiple fast-moving LEO satellites simultaneously due to latency, operational inefficiencies, and underutilized resources. While phased array antennas offer electronically steerable, multi-beam capabilities, their widespread adoption in ground stations is hindered by challenges in …

Exploring Lunar Ionosphere Characterization Through Multi-Cubesat Occultation With Ranging Technology And Radiation Environment Analysis, Yiyu Chang, Yuhsiu Tien, Chieh Lung, Jason Yu, Weichih Lin, Yihsuan Chou, Roger Tsai, Terry Chen, Yi Duann, Loren Chang

Small Satellite Conference

Characterizing the lunar ionosphere and radiation environment is critical for advancing both scientific knowledge and the practical requirements of future lunar missions. This mission proposes deploying dual satellites in lunar orbit to perform radio occultation (RO) measurements and validate the presence and behavior of the lunar ionosphere. By analyzing the phase differences of dual-frequency signals, the electron density can be measured, enabling both temporal analysis and spatial mapping of the lunar ionospheric structure. A thorough understanding of these environmental factors is essential for identifying suitable landing sites, designing resilient infrastructure, and ensuring the reliability of communication and navigation systems—key enablers …

Gram-Scale Chipsat Spacecraft For Light Sailing In Leo, Joshua Umansky-Castro, Matthew Hurford, Corbin Heywood, Grace Tang, Cameron Goddard, Jonathan Ma, Apurva Hanwadikar, Mason Peck, Andrew Filo, Alex Burke

Small Satellite Conference

Cornell University’s Alpha mission is a 1U CubeSat that deploys a retroreflective free-flying light sail in LEO. Mounted to the sail, and serving as its flight computers, are four ChipSats –gram-scale spacecraft assembled onto a single palm-sized PCB. These satellites collect and downlink data on the sail’s orbital position and attitude kinematics, communicating directly with low-cost ground stations around the globe. This paper introduces the ChipSat developed specifically for the Alpha mission launching in 2025. The new femto-satellite builds on previous-generation designs with a significant revamp of the RF communications. This paper provides an overview of the as-flown ChipSat design …

Telemetry Handling & Extensible Satellite Environment For A Unified System (Theseus) For The Operation Of Onglaisat, Shunsuke Shimomura, Kuna Shitara, Yuki Kusano, Yojiro Yamashiro, Tomoki Mochizuki, Shunichiro Nomura, Takeshi Matsumoto, Akihiro Ishikawa, Yosuke Kawabata, Satoshi Ikari, Ryu Funase, Shinichi Nakasuka

Small Satellite Conference

The recent increase in small satellites and diverse satellite missions has heightened the need for flexible and highly reliable ground station software. However, most existing open-source ground station software is implemented with the entire system in mind, making it difficult to accommodate diverse missions. Even when accommodating diverse missions, it is necessary to edit configuration files with a wide range of descriptions or make internal service modifications. Furthermore, as the number of available ground station services increases, there is an urgent need for systems that can support a wider range of interfaces. In addition, modern satellite development requires flexible support …