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Articles 13891 - 13920 of 5202347
Full-Text Articles in Entire DC Network
First Generation Of Project A.S.P.I.R.E. – A 1u Cubesat Mission For Technology Demonstration And Student Involvement In New Zealand, Shuanghui Zhao, Shunxing Shi, Kristen Lian, Rose Peens-Hough, Arami Peens-Hough, Changrui Wang, Joowon Hwang, Jerry Sun, Edward Sun
First Generation Of Project A.S.P.I.R.E. – A 1u Cubesat Mission For Technology Demonstration And Student Involvement In New Zealand, Shuanghui Zhao, Shunxing Shi, Kristen Lian, Rose Peens-Hough, Arami Peens-Hough, Changrui Wang, Joowon Hwang, Jerry Sun, Edward Sun
Small Satellite Conference
MOTIVATION
A feasibility study conducted at an Auckland secondary school in December 2024 found strong interest in satellite-related learning. Following an outreach presentation, 63 students (Majority aged 15 - 18) completed a questionnaire, with an average interest rating of 4.86/5. The most popular subjects were Orbital Physics, Mathematics, Mechanical Engineering, and Electrical Engineering (fig. 1).
Investigation Of A Demonstration Mission For Three-Dimensional Remote Sensing Using “Structured Radio Waves” With Orbital Angular Momentum, Hisatoshi Kimura, Tsukasa Funane, Yosuke Tanabe, Miki Yonehara, Makoto Ito, Keigo Nakamura, Yasuyuki Miyazaki, Satoshi Ikari, Shinichi Nakasuka, Koichi Watanabe
Investigation Of A Demonstration Mission For Three-Dimensional Remote Sensing Using “Structured Radio Waves” With Orbital Angular Momentum, Hisatoshi Kimura, Tsukasa Funane, Yosuke Tanabe, Miki Yonehara, Makoto Ito, Keigo Nakamura, Yasuyuki Miyazaki, Satoshi Ikari, Shinichi Nakasuka, Koichi Watanabe
Small Satellite Conference
Background
- As a new radar technology for remote sensing, three-dimensional observation methods using electromagnetic waves with spatial phase distributions are being studied to obtain azimuth-angle information in addition to conventional radar measurements[1].
- We are considering the use of “structured radio waves”, which are formed by superposing two radio waves carrying orbital angular momentum (OAM), as radio waves with spatial phase distributions[2,3].
Purpose
- Evaluate the effects of satellite position and attitude errors on azimuth-angle estimation and clarify the requirements for a demonstration mission.
- Assess the feasibility and provide recommendations.
Launch Vehicle And Ground Infrastructure Development For Zero Launch Systems, Masahiro Kinoshita
Launch Vehicle And Ground Infrastructure Development For Zero Launch Systems, Masahiro Kinoshita
Small Satellite Conference
ZERO is a two-stage, orbital-class launch vehicle designed to provide flexible, affordable, and localized space access.
Microsat For Refueling Mission Demonstrator In Vleo, Gyusun Kim
Microsat For Refueling Mission Demonstrator In Vleo, Gyusun Kim
Small Satellite Conference
Recently, active research and technological development have been conducted on various mission application in VLEO(Very Low Earth Orbit) using MicroSat. However, the limited payload accommodation capability of MicroSat poses significant challenges for high optical resolution commercial or national-level practical missions. In contrast, satellites of 2,000 kg in size have performed well in low-Earth orbit for the very high optical resolution missions required so far (e.g., 30 cm-level resolution optical satellites) in 450 km ~ 600 km orbit altitude, but in order to meet the continuously increasing resolution requirements in the future optical imagery market (e.g., 15 cm-level resolution), the optical …
Mission Orientated Flight Software Development: Cubestep, Tirth Thakkar, Howard Lee, Viren Kumar, Maranda Laws, Shridhi Seth, Marco Maggia, Navid Nakhjiri
Mission Orientated Flight Software Development: Cubestep, Tirth Thakkar, Howard Lee, Viren Kumar, Maranda Laws, Shridhi Seth, Marco Maggia, Navid Nakhjiri
Small Satellite Conference
Small satellite teams often develop flight software and mission operations separately, leading to software behaviors that drift out of sync with ground procedures. To fix this, we present a co-design approach that directly links mission goals and operational procedures to the onboard flight software architecture. Demonstrated on the CubeSTEP-Cerberus mission using NASA’s F′ framework and FreeRTOS, our system maps mission intent into five constrained software states (Initialization, Safe, Idle, Experiment, and Transmit) guarded by automated health checks. This co-design strategy ensures the spacecraft acts autonomously to preserve its goals while strictly maintaining operator control over critical decisions.
Oxford Space Systems Deployable Wrapped Rib Antenna (Wra): Initial On-Orbit Results, Peter Ashworth, Samuel Puche, Yuki Tsutsui, Duncan Shepherd, Amool Raina, Chris Bee, Vincent Fraux, Alex Da Silva Curiel, Danilo De Almedia, Liam North, Andrew Haslehurst, Darren Jones
Oxford Space Systems Deployable Wrapped Rib Antenna (Wra): Initial On-Orbit Results, Peter Ashworth, Samuel Puche, Yuki Tsutsui, Duncan Shepherd, Amool Raina, Chris Bee, Vincent Fraux, Alex Da Silva Curiel, Danilo De Almedia, Liam North, Andrew Haslehurst, Darren Jones
Small Satellite Conference
Oxford Space Systems (OSS) has achieved significant advancements in space deployable antennas, enabling small-satellite constellations through their low mass, low launch volume and high RF performance. Launched in January 2026 on a Falcon 9 rocket, OSS have collaborated with SSTL on the CarbSAR mission in order to successfully demonstrate and validate the technology of the innovative deployable Wrapped Rib Antenna (WRA) in-orbit & its use in smallsat SAR.
The CarbSAR mission has been jointly funded by Oxford Space Systems, SSTL, Airbus Defence and Space, UKDI-DASA, DSTL and the National Security Strategic Investment Fund (NSSIF), within a long-term programme that also …
A Hybrid Architecture For Scalable High-Frequency Inflatable Reflectors For Small Satellites, Aman Chandra, Hina Suzuki, Shashank Verma, Zac Chen, Dustin Blanchard, Christopher Walker
A Hybrid Architecture For Scalable High-Frequency Inflatable Reflectors For Small Satellites, Aman Chandra, Hina Suzuki, Shashank Verma, Zac Chen, Dustin Blanchard, Christopher Walker
Small Satellite Conference
Space-based telecommunications and remote sensing increasingly demand large-aperture antennas capable of operating at high frequencies, specifically Ka-band and above. While inflatable membrane structures offer the low mass and compact stowage necessary to deploy large reflectors in excess of two meters from small satellite platforms, their adoption has been hindered by the difficulty of maintaining precise surface geometry. To establish a viable pathway for these high-frequency applications, the University of Arizona and Freefall Aerospace have developed a hybrid tensioning and deployment mechanism, validated on a one-meter lenticular reflector. This system decouples boundary tension from internal pressure, using a novel adaptive pre-tensioning …
Planet's Next Generation Evolution Of The High Speed Radio: 10 Gbps Smallsat Radio, David Nemeth, Kiruthika Devaraj, Varun Sharma, Timothy Kordas, Gil Michael, Stefan Turkowski, Abhra Dasgupta
Planet's Next Generation Evolution Of The High Speed Radio: 10 Gbps Smallsat Radio, David Nemeth, Kiruthika Devaraj, Varun Sharma, Timothy Kordas, Gil Michael, Stefan Turkowski, Abhra Dasgupta
Small Satellite Conference
Planet is a vertically integrated aerospace and data analytics company that operates the world’s largest commercial fleet of remote sensing satellites. Our mission is to image the whole world every day, and make change visible, accessible, and actionable. We have launched over 600 satellites and built up an automated mission control and ground station infrastructure to monitor and control the satellites, and download the imagery data. Planet’s agile aerospace philosophy of rapid prototyping, iteration, and adaptation of the latest commercial-off-the-shelf (COTS) technology has allowed for continuous improvements in data throughputs on our High Speed Downlink radio. Planet’s HSD2 achieves greater …
Modular, Scalable Electroadhesive Technology For Rapid Response Satellite Servicing And De-Orbit, Kalia Crowder, Victor Agüero
Modular, Scalable Electroadhesive Technology For Rapid Response Satellite Servicing And De-Orbit, Kalia Crowder, Victor Agüero
Small Satellite Conference
Building on previous surface attachment testing and a study of the Cambrian Works Space Payload for Inertial Despin Efficient Effects (SPIDEE) architecture carried out under AFRL support, this work presents a modular, scalable electroadhesive attachment architecture enabling rapid-response satellite servicing and de-orbit missions. Prior test and analysis campaigns provided quantified performance validation across the small satellite size range, from 3U CubeSats to ESPA-class platforms, demonstrating the scalability required for diverse time-critical servicing scenarios.
Testing validated performance under representative on-orbit conditions and dynamic scenarios. Attachment force measurements across spacecraft materials representing aluminum bus structures, composite panels, multi-layer insulation, and solar cells …
A Survey Of The State Of The Art In Multi-Spacecraft, Multi-Agent Swarms, Caleb Adams, Trey Smith, Aaron Woodard, Ellemieke Van Kints, Brian Kempa, Jeremy Frank
A Survey Of The State Of The Art In Multi-Spacecraft, Multi-Agent Swarms, Caleb Adams, Trey Smith, Aaron Woodard, Ellemieke Van Kints, Brian Kempa, Jeremy Frank
Small Satellite Conference
The Next-Generation Multi-Agent Swarm (NGS) Study conducted by NASA’s Ames Research Center for NASA’s Space Technology Mission Directorate (STMD) has developed a comprehensive understanding of emerging multi-agent swarm capabilities for applications in cislunar and lunar space. This paper addresses specific shortfalls identified by STMD, including intelligent multi-agent constellations, autonomy, edge computation, position, navigation, and timing for small spacecraft, and small spacecraft propulsion. This paper surveys the current state of the art in technology areas relevant for the next-generation multi-agent swarm design. Our primary focus is on surveying relevant deployed space systems, supplemented with selective analysis of relevant proposed missions and …
Design, Qualification, And Implementation Of Modular Spacecraft Radio Testing Enclosures For Small Satellite Missions, Dexter Stewart
Design, Qualification, And Implementation Of Modular Spacecraft Radio Testing Enclosures For Small Satellite Missions, Dexter Stewart
Small Satellite Conference
As small satellite missions evolve, spacecraft platforms increasingly integrate radio-frequency (RF) antennas to support telemetry, command, and inter-satellite communication links that must be verified following full system integration. Recent changes in launch site safety policy, most notably SpaceX’s ban on over-the-air (OTA) testing, have created a critical gap in the ability to qualify spacecraft communication systems during testing at the launch site. This paper presents the design, qualification, and implementation of modular RF containment enclosures, known as ’antenna hats’, developed to enable safe, non-OTA testing of fully integrated small satellites. The antenna hats are self-contained enclosures that interface directly with …
Distribution Of Urinary Calculi And Its Association With Clinical And Laboratory Findings In Dogs And Cats With Stone Analysis At Chulalongkorn Animal Teaching Hospital, Thailand (2020-2024), Tanattha Ladabornvidhaya, Natkrita Baikloy, Theaparak Thipjaroen, Parapond Kongrakchang, Warisara Kaechaiya, Sumonwan Chamsuwan, Monkon Trisiriroj, Chollada Buranakarl
Distribution Of Urinary Calculi And Its Association With Clinical And Laboratory Findings In Dogs And Cats With Stone Analysis At Chulalongkorn Animal Teaching Hospital, Thailand (2020-2024), Tanattha Ladabornvidhaya, Natkrita Baikloy, Theaparak Thipjaroen, Parapond Kongrakchang, Warisara Kaechaiya, Sumonwan Chamsuwan, Monkon Trisiriroj, Chollada Buranakarl
The Thai Journal of Veterinary Medicine
Urinary calculi are commonly encountered in veterinary practice; however, information regarding their distribution of stone that underwent analysis and associated clinical findings remains limited. This study investigated the distribution of urolithiasis and the associations between stone types and clinical and laboratory findings in dogs and cats presented to the Chulalongkorn Small Animal Teaching Hospital between 2020 and 2024. The three most common stone types in both species were calcium oxalate (CaOx), struvite, and urate, with relatively stable trends over the 5-year period. Small-breed dogs had a higher risk of developing CaOx urolithiasis than medium-breed dogs (OR = 10.4, 95% CI …
Development, Analysis, And Qualification Of A Hinge And Hdrm Assembly For Small Satellite Deployable Probes, Josh Taylor
Development, Analysis, And Qualification Of A Hinge And Hdrm Assembly For Small Satellite Deployable Probes, Josh Taylor
Small Satellite Conference
Small satellites commonly utilize deployable systems to expand their space environment sensing and power generation capabilities. Sensing the space environment is required for certain missions, as it provides information about space weather events such as scintillation and solar flares. To accurately measure the space environment, the probes must be placed away from the spacecraft while in orbit. This paper presents the development, analysis, and qualification of a hinge and Hold-Down and Release Mechanism (HDRM) assembly for deployable space weather probes. These two mechanisms were developed as an assembly to be lightweight, compact, and reliable for deploying space weather probes. The …
Development Of A Low-Cost Uas Air Sampler For Multi-Point Aerosol Collection, Avinash Muthu Krishnan, Kevin A. Adkins, Marc D. Compere, David Zink, Emel Sen-Kilic, Justin Fratto, Kayla D. Taylor
Development Of A Low-Cost Uas Air Sampler For Multi-Point Aerosol Collection, Avinash Muthu Krishnan, Kevin A. Adkins, Marc D. Compere, David Zink, Emel Sen-Kilic, Justin Fratto, Kayla D. Taylor
ISARRA 2026
This work describes the development of a low-cost uncrewed aircraft system (UAS)-mounted air sampler for collecting multiple discrete aerosol samples during a single flight. The system uses a liquid impinger approach in which ambient air is drawn through a collection liquid to capture soluble aerosol material. Multiple sterile collection tubes and a solenoid-controlled flow path allow the sampler to collect separate samples at different locations without landing between collections.
A key design issue in a multi-sample system is contamination between samples. To address this, the payload includes a purge step and a flow layout designed to reduce carryover in shared …
The Citizens Bank Of Jacksonville, From Eartha M. M. White To Furchgotts Co.
The Citizens Bank Of Jacksonville, From Eartha M. M. White To Furchgotts Co.
Eartha M. M. White Textual Material
Document: Cancelled check - The Citizens Bank of Jacksonville. Pay to the order of Furchgotts Co., twelve dollars. Handwritten note on front: Cash. Date: June 18, 1929
Beyond Parametric Adaptation: Periodic Redesign For Reaction Wheel Degradation In Precision Pointing Cubesats, Bruno Ingrao
Beyond Parametric Adaptation: Periodic Redesign For Reaction Wheel Degradation In Precision Pointing Cubesats, Bruno Ingrao
Small Satellite Conference
CubeSat missions increasingly require sustained science-grade precision pointing over long durations. Although sub-arcsecond line-of-sight (LoS) stability is achievable, maintaining this performance is challenged by nonlinear, speed-dependent, and time-varying reaction wheel behavior. As actuator degradation progresses from beginning-of-life (BOL) to end-of-life (EOL), model-plant mismatch can lead to significant pointing degradation and potential loss of mission capability. This work investigates the limitations of fixed-gain and parametric adaptive control under degraded actuator conditions and proposes a periodic identification and controller redesign framework. The approach detects persistent model mismatch using innovation-based consistency and performance metrics, triggers on-orbit identification, and updates the actuator model using …
Trustless Cross-Chain Derivation Of Ipfs Content Identifiers Via Zero-Knowledge Proofs, Ryley Ohlsen, Lindsay Gilbert, Matthew Etre
Trustless Cross-Chain Derivation Of Ipfs Content Identifiers Via Zero-Knowledge Proofs, Ryley Ohlsen, Lindsay Gilbert, Matthew Etre
Defensive Publications Series
A method by which an application on one EVM-compatible blockchain can obtain a cryptographically-verified IPFS content identifier (CID) for content whose canonical bytes live on a different EVM-compatible blockchain (or are stored compressed on any chain), without relying on an oracle, a governance-managed attestation, or a trusted relayer. A zero-knowledge proof of correct execution of an on-chain-IPFS-importer computation (see companion disclosure, “On-Chain Reconstruction of IPFS Content Identifiers from EVM-Resident Content-Addressed Data”) is generated off-chain and verified on-chain in constant time, regardless of the size of the underlying content.
Book Review: Judicial Originalism As A Byproduct Of An Overly Difficult Amendment Process: Jill Lepore's We The People, Charles Britton
Book Review: Judicial Originalism As A Byproduct Of An Overly Difficult Amendment Process: Jill Lepore's We The People, Charles Britton
ConLawNOW
This essay reviews the book by Jill Lepore, We the People: A History of the U.S. Constitution, winner of the 2026 Pulitzer Prize for history. It explains how Lepore examines the history of constitutional amendment—both successes and failures—to argue that frequent amendment was the democratic intent of the Framers. And shows how this amendment philosophy contradicts the originalism of the current Supreme Court.
Framework For Design, Modelling, And Qualification Of Phase Change Material Heat Sinks For Small Satellites, Daniel Kichma
Framework For Design, Modelling, And Qualification Of Phase Change Material Heat Sinks For Small Satellites, Daniel Kichma
Small Satellite Conference
The increasing use of high-power hardware in small satellites presents a critical thermal management challenge. Phase Change Material (PCM) heat sinks provide passive thermal control for transient heat loads by storing thermal energy as latent heat during melting, maintaining near-constant temperatures. This creates a thermal buffer that lowers peak heat fluxes and reduces the required radiative surface area. A PCM heatsink was required for thermal control of a payload on an upcoming mission at the Space Flight Laboratory (SFL). This motivated the development of in-house PCM capabilities to enable mission-specific designs at lower cost and shorter schedules. This paper presents …
Radma: Resource-Aware, Dynamic Deployment Of Ml Architectures On An Edge Tpu In Space, Robert Rathert
Radma: Resource-Aware, Dynamic Deployment Of Ml Architectures On An Edge Tpu In Space, Robert Rathert
Small Satellite Conference
As the number of Space Vehicles (SVs) orbiting Earth grows, downlink bitrate bottlenecks necessitate a shift to Orbital Edge Computing (OEC). Size, Weight, and Power, and Cost (SWaP-C) limit onboard Machine Learning (ML) autonomy, and State-of-the-Art (SotA) systems deploy static ML models that do not adapt to dynamic orbit conditions. This work proposes and evaluates RADMA, a resource-aware framework that selects Neural Network (NN) models in response to changing latency and energy constraints. We quantify the performance of RADMA on an open-hardware picosatellite payload that hosts a Google Coral Edge Tensor Processing Unit (TPU). Orbit simulation and modeling predict processing …
Validated Lie Group Variational Integrator-Based Simulator For Passive Magnetic Attitude Control Of The Gasrats Cubesat, Truman T. Abbe
Validated Lie Group Variational Integrator-Based Simulator For Passive Magnetic Attitude Control Of The Gasrats Cubesat, Truman T. Abbe
Small Satellite Conference
Passive magnetic attitude control (PMAC) systems are selected for integration in CubeSat designs on account of their simplicity and lack of power consumption. These systems function by simultaneously dissipating a satellite’s rotational kinetic energy as heat and orienting it according to the Earth’s magnetic field. This process is critical for establishing steady-state attitude, a stable rotational state required for conducting mission operations and enabling downlink to ground stations. Comprehensive attitude simulations are necessary for confirming the reliability of a PMAC system to provide timely attitude convergence for a wide range of deployment velocities and orientations. An attitude damping phase precedes …
66: Revelation Manuscript, Jack J. Blanco
66: Revelation Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of Revelation is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
65: Jude Manuscript, Jack J. Blanco
65: Jude Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of Jude is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
64: Iii John Manuscript, Jack J. Blanco
64: Iii John Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of III John is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
63: Ii John Manuscript, Jack J. Blanco
63: Ii John Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of II John is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
62: I John Manuscript, Jack J. Blanco
62: I John Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of I John is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
61: Ii Peter Manuscript, Jack J. Blanco
61: Ii Peter Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of II Peter is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
60: I Peter Manuscript, Jack J. Blanco
60: I Peter Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of I Peter is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.
59: James Manuscript, Jack J. Blanco
59: James Manuscript, Jack J. Blanco
The Clear Word Manuscript
This handwritten manuscript of James is part of the original biblical paraphrase manuscript that later became The Clear Word, authored by Dr. Jack J. Blanco.