Digital Commons Network^™

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

Small Satellite Conference

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

Systems Progress Overview Of Rosisat: The Radiation Orbital Shielding Investigation Satellite, Chase Patterson, Jacob Blanton, Jayden Mcdonald, Kylie Nager, Colson Walker, Francisco Crespo Cutillas

Small Satellite Conference

Exposure to space weather in the Low Earth Orbit (LEO) space weather environment poses significant challenges to both the integrity and longevity of orbital hardware, as well as the health of astronauts, driving the necessity for improved means of radiation shielding for future manned and unmanned missions. With a 1U CubeSat formfactor, ROSISat is a planned LEO mission that aims to characterize the radiation shielding capabilities of seven candidate materials. By comparing the shielding performance of each composite and constituent material, ROSISat will place a specific focus on correlating how molecular structure influences radiation shielding. Further, current simulations lack the …

Reacquiring Satellites After Unknown Maneuvers In Sensor Blind Spots: A Physics-Informed Behavioral Framework For Closed-Loop Custody Recovery, Naushad Rahman, Niha Agarwalla, Hardik Patel

Small Satellite Conference

Operational problem

After a maneuver during a sensor blind spot, a pre­-gap catalog state may no longer be operationally sufficient. A null look at GS2 must become evidence for where the object could be­ – and where to task next – before access expires.

Scaling Space Power For Small Satellites: Why Manufacturing Capacity Now Matters As Much As Efficiency, Mpower Technology

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

The Quantum Cubesat: A Perspective For Quantum Technology In Orbit, Natalie Pearson, Andrew Kelly, Curtis Talbot, Colin Aitken, Kevin Quillen, Sandy Provan

Small Satellite Conference

Motivation

The ability to measure, control and exploit quantum effects has shown significant potential to outperform classical devices across a variety of applications in computing, sensing and communication. However, quantum devices today typically depend equipment that is large, heavy, expensive and delicate. Bringing quantum capability to space requires a relentless focus on miniaturisation, ruggedisation and applicability. Focusing engineering efforts on the most promising technologies to realise their benefits in orbit is a crucial step in this process.

Validation Of Steering Law For A 4-Variable-Speed Single-Gimbal Control Moment Gyroscope Pyramid Cluster Via Spherical Air-Bearing Testbed, Kai Kuo Liao, Chih Ta Wu, Jen Hao Cheng, Po Hsun Yen, Shang Jung Lee

Small Satellite Conference

• VSCMG: wheel speed is commanded with gimbal rate — the extra DOF lets the cluster slide past singularities.
• HIL: a Helmholtz cage replays the on-orbit field and a solar simulator sets the Sun line.
• This work: HIL validation of a weighted-pseudoinverse steering law, 4-unit pyramid.

University Ground-Station-As-A-Service: Promoting Space It Education And University Collaboration, Daniel Freburg, Will Lewis, Charles Edamala, Phoenix Alpine

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Vpx/Sosa Systems: Enabling Multi-Vendor Interoperability, Novo Space

Small Satellite Conference

Poster presented at the 2026 Small Satellite Conference

Zerodur®: Tailoring Opportunities For Your Thermal Environment And Second-Order Optimum Factors, Jesse Bonfeld, Dustin Ruth, Florian Gollier, Janina Krieg, Thomas Westerhoff, Tony Hull, Jacqueline Caraballo

Small Satellite Conference

Poster Presented at the 2026 Small Satellite Conference

Reinventing The Reaction Wheel, I. Penchev, N. Andrada

Small Satellite Conference

Rapid growth of microsatellite missions and constellations in the 10–600 kg class is increasing the demand for scalable, high-performance attitude control solutions. Advanced payloads for Earth Observation, Synthetic Aperture Radar, complex science missions, and geolocation systems require:

• Low microvibration performance
• Precise pointing stability
• High angular momentum capacity
• Reliable across mission lifetimes

Space Inventor is qualifying a new generation of 1 Nms-class reaction wheels optimized for microsatellite platforms. The innovative mechanical design, combined with manufacturing-aware system design, unlocks expanded performance and mission opportunities for microsatellites and constellations.

Satellite Autonomous Launch Assembly (Satlass): Cold Gas Propulsion System Testing, Anthony Todisco Jr., Jaden Caradine, Justin Della, Essence Howard, Colin Mccaughey, Andrew Hawks, Alexander Kushto, Javier Narvaez, Gabriella Colon O'Hara, Franyerson Lopez Ochoa, Elizabeth Ptak, Diana Tormo, Francisco Crespo Cutillas, Sean Crouse, Lary Finberg

Small Satellite Conference

Project SATLASS plans to become one of the first cold gas propelled CubeSat Deployers used. Using Nitrogen gas, SATLASS will be able to place multiple CubeSats into customizable orbits autonomously. A modular housing unit will allow for 3-1U CubeSats to 1-3U CubeSat to ride along with SATLASS through Low Earth Orbit.

Leveraging Persistent L-Band Leo-To-Geo Relays For The Orchestration Of High-Bandwidth Optical Inter-Satellite Links, Jonathan Maier, Skylar A. Cox

Small Satellite Conference

As the already tremendous demand for data transfer in Low Earth Orbit (LEO) grows, Free-Space Optical (FSO) communication has emerged as a critical capability due to high data rates and inherent resilience attributes. However, the operational complexity of FSO, specifically the Pointing, Acquisition, and Tracking (PAT) process, requires significant operational planning. The narrow beamwidth of optical terminals requires precise spatial coordination, resulting in latency during link establishment, heavy reliance on scheduled ground-based commanding, and an impediment to agile, responsive, and ad hoc operations.

This paper presents a novel orchestration architecture utilizing Viasat’s L-band space relay network as a persistent, always-on …

Evaluating Performance Of Hardware-Accelerated Vessel Detection Algorithms, Michael Tietz, John Warner, Quinton Davidson, Douglas Carssow

Small Satellite Conference

Earth observing satellites contribute to the monitoring of maritime activity by enabling large-scale coverage of open water. For example, spacecraft data can be used to monitor and combat Illegal, Unreported, and Unregulated (IUU) fishing that occurs in coastal and international waters across the globe. However, information latencies limit the utility of space-based sensors for operational users who need real-time situational awareness. These limitations are especially pronounced for small spacecraft with limited power generation and downlink capabilities. In recent years, the devices and tools that enable edge computing and near real-time downlink from small spacecraft have improved substantially. Equipped with these …

Dynaband: Context-Aware Dynamic Band Selection For Onboard Hyperspectral Processing In Small Satellites, Rishigesh Jayananth, Brasen Sheeh

Small Satellite Conference

Hyperspectral small satellites now collect far more data than they can return to the ground. A single acquisition spans tens to hundreds of spectral bands, yet the downlink window on one pass carries only a fraction of it, so operators are forced to drop scenes, bin bands coarsely, or store data that never reaches the ground. Much of this waste is avoidable. When the task is known before the spacecraft images, whether to map water, monitor vegetation, or pick out a mineral signature, only a handful of bands actually carry the answer; the rest is paid for in downlink and …

Metadata-Conditioned Dark-Frame Modelling And Hsdr-Scanfusion Denoising: A Physics-Informed Independent Tool For Low-Cost Hyperspectral Small-Satellite Calibration, Nooh Adnan, Kyaw Thiha, Raffael Gil Dela Cruz, Li Cheng Zheng, Faijul Amin, Areeba Khan, Sameha Tasnim, Sung Jegal, Yunhan Bao, Iliya Shofman

Small Satellite Conference

Hyperspectral imaging in the shortwave-infrared spectrum is valuable for orbital Earth observation, but its use on low-cost, resource-constrained small satellites is limited by thermally dependent dark current, fixed-pattern noise, and intermittent access to matched calibration frames. Traditional mitigation through active cooling, shutters, or frequent dark-frame acquisition can be difficult to accommodate within small-satellite mass, power, volume, and operations budgets. This paper presents a physics-informed independent calibration tool that reconstructs condition-matched dark response from acquisition metadata rather than relying on hardware-heavy calibration at every operating point. The framework combines a stochastic dark-noise simulator, a metadata-conditioned neural dark operator that predicts spectral-spatial …

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

Small Satellite Conference

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

Development Of Wavelength-Division-Multiplexed All-Optical Relays For Low-Earth Orbit Free-Space Optical Communication Networks, Travis Jones, Justin Cook, Chris Krush, Doruk Engin, Keith G. Petrillo

Small Satellite Conference

In this work, we designed, built, and tested an all-optical relay amplifier to enable a space-based all-optical backbone for laser communications networks. The design sought to optimize links for LEO-based networks incorporating appropriate span lengths and optical terminal specifications. We incorporate an add-drop multiplexer for rerouting signals and designed the system to be flexible over span lengths with a nominal range of 1,800 km. We performed several tests of the nominally 60 dB gain amplifier to assess link dynamics unique to free space optical communications (FSOC) including the impact of pointing jitter, nonlinearities, gain flattening, and wide-band filters on an …

Delay/ Disruption Tolerant Networking In Cislunar Space, Sara Garcia-Beech, Rebecca Besser, Elizabeth Geist, Theresa Beech, Mike Palsson, Krishnan Narayanan, Ben Anderson

Small Satellite Conference

DTN (Delay/Disruption Tolerant Networking) is at foundation of NASA's LunaNet architecture, which will enable the robust communications, navigation, and networking capabilities needed to establish a long-term presence on the Moon. DTN is a network architecture composed of several different protocols that are designed to provide internetworking functionality and standardized multi-hop, end-to-end data delivery in highly stressed environments that are not optimal for traditional Internet Protocols. Bundle Protocol (BP) version 7, a store-and-forward protocol intended to run at the application layer on top of convergence layer protocols, provides the key delay tolerance functionality of DTN and is designed to handle intermittent …

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

Small Satellite Conference

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

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

Let’S Give The Fsck Up On Secded, Heather M. Quinn, Andrew Pineda, Gary Swift

Small Satellite Conference

Many space systems use error correcting codes (ECC) for handling radiation-induced upsets in memories. The most used ECCs are Hamming and Hsaio, which are single-error correction/double-error detection (SECDED) codes. The widespread use of these codes can lead to a dangerous overestimation of system reliability. Instead these codes are one of the best documented methods for microprocessor-based system crashes, due to uncorrectable faults. Less well documented is how these codes can lead to silent data corruption caused by miscorrections, where multiple errors are detected as a single error and corrected erroneously.

ECCs have always been sensitive to time-dependent errors, where SEUs …

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

Small Satellite Conference

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

Demonstration Of Bidirectional Tracking And Data Transfer With The Cubeisl Optical Communication Terminal, Jan Hildebrand, Hannes Zeihsel, René Rüddenklau, Jorge Rosano Nonay, Lukas Rodeck, Olman Quiros Jimenez

Small Satellite Conference

This paper presents the experimental results of a free-space optical link validating the capabilities of two integrated CubeISL terminals. The campaign serves as a verification of the tracking, pointing and acquisition of the terminals before launch of the CubeISL mission. The link was conducted over a distance of 6600 m between the rooftop of the DLR Institute of Communication and Navigation in Oberpfaffenhofen and a 80 m high radio tower in Schöngeising. To ensure robust link establishment, the system employed a Pointing, Acquisition, and Tracking scheme utilizing both a 10 kHz modulated beacon for initial acquisition and a Continuous Wave …

Design And Qualification Of A Compact, Deployable Dual-Monopole Antenna System For Remote Sensing Microsatellites, Alexander J. Murphy, Bryan Johnston-Lemke, Robert E. Zee

Small Satellite Conference

Spacecraft conducting signals intelligence (SIGINT) missions require highly capable radio-frequency (RF) payloads. While the larger 80 kg-class platforms offer increased payload capacities, strict internal volume limitations persist. These constraints sometimes require stowing instruments, such as the dual-monopole Very High Frequency (VHF) antenna presented in this work, directly beneath the solar wings. This requirement has imposed a strict height constraint on the VHF antenna, mandating a highly compact and reliable deployment mechanism that avoids snagging or jamming during deployment. 

This paper presents the mechanism design and qualification test plan of a novel, deployable dual-monopole VHF antenna system designed to increase satellite …

Recovery Of Grus-1e From Magnetic Torquer Loss Using Data-Driven Open-Loop Attitude Steering, Nader Ganaba, Takanori Iwata, Minoru Kurata

Small Satellite Conference

In typical low Earth orbit (LEO) operations, the inability to remove excess angular momentum often leads to the decommissioning of a satellite. This paper presents the on-orbit recovery of GRUS-1E, a hundred kg class Earth observation satellite in Axelspace Corporation’s GRUS-1 constellation. The recovery followed the permanent loss of magnetic torquer commanding capability, which in turn disabled the satellite’s nominal reaction wheel momentum unloading. In addition, the satellite experienced persistent disturbance torques that significantly exceeded the combined contributions predicted by standard models, including gravity gradient, solar radiation pressure, aerodynamic drag, and the estimated residual magnetic dipole moment. The magnitude of …

The Genesis Of The Annual Usu Conference On Small Satellites, Rex Ridenoure, Alex Da Silva Curiel, Martin Sweeting

Small Satellite Conference

On this milestone of marking the 40^th SmallSat conference, this paper provides a capsule summary of how it all started in 1987, and why. 

By January 1986, Utah State University was actively involved with NASA’s Space Shuttle program, which from April 1981 through mid-January 1986 had notched 24 successful missions in a row, including nine in 1985. Missions were starting to appear routine, and the manifest was full for many dozens of future missions. 

The Shuttle’s Get Away Special (GAS) secondary payload program had become quite popular within academic, government and commercial sectors, and through 1985 six dozen separate …

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

Small Satellite Conference

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

A Smallsat In Vleo: The Orion Kraken Approach, Chad Fish, Crystal Frazier, Sun-Hee Goldsberry, Katie Nyland, Will Armijo, Raj Patel, Elijah Vance, Adam Reynolds, Nathan Tipton, Kevin Quintana, Sam Clowes, Rachel Stutz, Keith Underwood, Jared Stromberg, Justin Berger, Erich Hoover, Andrew Irvine, Ali Wise, Christian Frazier, Derek Taylor, Kong Yang, Tracy Cueto, Wes Leong, Greg Ushomirsky, Charles Swenson, Paul Bernhart, Ron Reedy, Tim Minton, Mitchell Weins, Kent Frankovich

Small Satellite Conference

The Orion Space Solutions' Kraken Mission, sponsored by DARPA and implemented by a science and engineering team led by Orion Space Solutions, will make in-situ and remote sensing space weather observations from Very Low Earth Orbit (VLEO). The mission instrument suite will include Langmuir Probes, RF Impedance Probes, HF Sounders, Atomic Oxygen Sensors, Science Magnetometers, Floating Potential Probes, and Science Accelerometers. Long-term (approximately 4-6 month lifetime), repeated measurements of plasma density and other plasma and neutral parameters in this region are very rare, and the Kraken data is expected to contribute considerably to space weather and science modeling of VLEO. …

The Cospar-1 Spacecraft: Advancing Space Science And Capacity Building Through International Collaboration, Amal Chandran, Hex20 Ltd., Carlos Gabriel, Loren C. Chang

Small Satellite Conference

The Committee on Space Research (COSPAR) is the world's leading organization for advancing space science. The COSPAR Panel for a Constellation of Small Satellites (PCSS) was assembled in 2020 to examine how emerging CubeSat and small satellite technology could help solve outstanding questions in Space Weather, Earth Climate change, and Radiation Belt studies through constellations of miniature spacecraft. The COSPAR-1 spacecraft is a 3U CubeSat carrying a Solar Spectral Sensor from the Laboratory for Atmospheric and Space Physics (LASP) at the University of Colorado Boulder to observe solar output across the UV-to-IR spectrum, an Earth Radiation Sensor from LATMOS in …

The Landolt Mission Payload: An Artificial Star For Precision Astronomy, Peter Pachowicz, Peter Plavchan, Gabrielle Belle, Jay Deorukhkar, Philip Cunio, Eliad Peretz, John Mather, Peter Kurczynski, Angelle Tanner, Susana Deustua, Brian Alberding, Joseph Rice, Thomas Michaud-Baeyens, Jean-Thomomas Landry, Marc-Andre Boucher, David Ciardi, Mike Lund, Justin Albert, Greg Alderling, Brian Stalder, Daniel Stevens, Jamie Tayar, Daniel Kuesters, Tabetha Boyajian

Small Satellite Conference

The Landolt Mission represents a significant advancement in space-based instrumentation, serving as NASA’s first hybrid space mission. Central to the mission is a smallsat deployed in Geostationary Orbit (GEO), carrying the SI Traceable Absolute Radiometer [STAR] comprised of two Laser Instruments (LI) and an Element Wheel technology demonstrator. The LI utilizes six specialized Laser Trays to project SI-calibrated light beams at various wavelengths into ground telescopes. By creating a stable, SI-traceable calibration source, the Landolt mission aims to provide an unprecedented level of precision in astronomical observations. These advancements are expected to facilitate transformative discoveries in exoplanet host stars, supernova …

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 …