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        "authors": [
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        "abstract": "A mission out of the planetary system, launched about the year 2000, could provide valuable scientific data as well as test some of the technology for a later mission to another star. Primary scientific objectives for the precursor mission concern characteristics of the heliopause, the interstellar medium, stellar distances (by parallax measurements), low-energy cosmic rays, interplanetary gas distribution, and the mass of the solar system. Secondary objectives include investigation of Pluto. The mission should extend to 400-1000 AU from the sun. A heliocentric hyperbolic escape velocity of 50-100 km/sec or more is needed to attain this distance within a reasonable mission duration (20-50 years). The trajectory should be toward the incoming interstellar gas. For a year 2000 launch, a Pluto encounter and orbiter can be included. A second mission targeted parallel to the solar axis would also be worthwhile. The mission duration is 20 years, with an extended mission to a total of 50 years. A system using one or two stages of nuclear electric propulsion (NEP) was selected as a possible baseline. The most promising alternatives are ultralight solar sails or laser sailing, with the lasers in earth orbit, for example. The NEP baseline design allows the option of carrying a Pluto orbiter as a daughter spacecraft.",
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        "abstract": "The Environmental Control and Life Support System (ECLSS) is a Freedom Station distributed system with inherent applicability to extensive automation primarily due to its comparatively long control system latencies. These allow longer contemplation times in which to form a more intelligent control strategy and to prevent and diagnose faults. The regenerative nature of the Space Station Freedom ECLSS will contribute closed loop complexities never before encountered in life support systems. A study to determine ECLSS automation approaches has been completed. The ECLSS baseline software and system processes could be augmented with more advanced fault management and regenerative control systems for a more autonomous evolutionary system, as well as serving as a firm foundation for future regenerative life support systems. Emerging advanced software technology and tools can be successfully applied to fault management, but a fully automated life support system will require research and development of regenerative control systems and models. The baseline Environmental Control and Life Support System utilizes ground tests in development of batch chemical and microbial control processes. Long duration regenerative life support systems will require more active chemical and microbial feedback control systems which, in turn, will require advancements in regenerative life support models and tools. These models can be verified using ground and on orbit life support test and operational data, and used in the engineering analysis of proposed intelligent instrumentation feedback and flexible process control technologies for future autonomous regenerative life support systems, including the evolutionary Space Station Freedom ECLSS.",
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        "title": "The Controlled Ecological Life Support Systems (CELSS) research program",
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        "authors": [
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        "abstract": "The goal of the Controlled Ecological Life Support Systems (CELSS) program is to develop systems composed of biological, chemical and physical components for purposes of human life support in space. The research activities supported by the program are diverse, but are focused on the growth of higher plants, food and waste processing, and systems control. Current concepts associated with the development and operation of a bioregenerative life support system will be discussed in this paper.",
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        "title": "The Need for Fusion Propulsion",
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        "authors": [
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        "abstract": "Fusion propulsion is inevitable if the human race remains dedicated to exploration of the solar system. There are fundamental reasons why fusion surpasses more traditional approaches to routine crewed missions to Mars, crewed missions to the outer planets, and deep space high speed robotic missions, assuming that reduced trip times, increased payloads, and higher available power are desired. A recent series of informal discussions were held among members from government, academia, and industry concerning fusion propulsion. We compiled a sufficient set of arguments for utilizing fusion in space. If the U.S. is to lead the effort and produce a working system in a reasonable amount of time, NASA must take the initiative, relying on, but not waiting for, DOE guidance. In this talk those arguments for fusion propulsion are presented, along with fusion enabled mission examples, fusion technology trade space, and a proposed outline for future efforts.",
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        "selectionNote": "Curated as an advocacy-oriented historical synthesis of the energy, exhaust-velocity, payload, trip-time, and power arguments used to motivate fusion propulsion research.",
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        "curationTopic": "fusion propulsion",
        "evidenceBoundary": "NTRS lists open full text, but the preprint's assertion that fusion propulsion is inevitable is not treated as evidence, and no engineering demonstration is implied. It is argument history, not claim validation."
      }
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    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20150008371",
      "title": "Effects of Extreme Obliquity Variations on the Habitability of Exoplanets",
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      "snapshot": {
        "id": "ntrs-20150008371",
        "title": "Effects of Extreme Obliquity Variations on the Habitability of Exoplanets",
        "url": "https://ntrs.nasa.gov/citations/20150008371",
        "topic": "destinations-astrobiology",
        "year": 2014,
        "publishedAt": "2014-03-10T00:00:00.0000000+00:00",
        "authors": [
          "Armstrong, J. C.",
          "Barnes, R.",
          "Domagal-Goldman, S.",
          "Breiner, J.",
          "Quinn, T. R.",
          "Meadows, V. S."
        ],
        "publisher": "Mary Ann Liebert, Inc.",
        "resourceType": "Reprint (Version printed in journal)",
        "access": "open full text",
        "abstract": "We explore the impact of obliquity variations on planetary habitability in hypothetical systems with high mutual inclination. We show that large-amplitude, high-frequency obliquity oscillations on Earth-like exoplanets can suppress the ice-albedo feedback, increasing the outer edge of the habitable zone. We restricted our exploration to hypothetical systems consisting of a solar-mass star, an Earth-mass planet at 1 AU, and 1 or 2 larger planets. We verified that these systems are stable for 108 years with N-body simulations and calculated the obliquity variations induced by the orbital evolution of the Earth-mass planet and a torque from the host star. We ran a simplified energy balance model on the terrestrial planet to assess surface temperature and ice coverage on the planet's surface, and we calculated differences in the outer edge of the habitable zone for planets with rapid obliquity variations. For each hypothetical system, we calculated the outer edge of habitability for two conditions: (1) the full evolution of the planetary spin and orbit and (2) the eccentricity and obliquity fixed at their average values. We recovered previous results that higher values of fixed obliquity and eccentricity expand the habitable zone, but we also found that obliquity oscillations further expand habitable orbits in all cases. Terrestrial planets near the outer edge of the habitable zone may be more likely to support life in systems that induce rapid obliquity oscillations as opposed to fixed-spin planets. Such planets may be the easiest to directly characterize with space-borne telescopes.",
        "keywords": [
          "habitability of exoplanets",
          "exoplantes",
          "extreme obliquity variations"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “Effects of Extreme Obliquity Variations on the Habitability of Exoplanets” covers habitability of exoplanets, exoplantes, extreme obliquity variations; it materially informs GShips work on planetary habitability modeling.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "planetary-habitability-modeling",
        "evidenceBoundary": "NTRS provides open full text, but this reprint (version printed in journal) was screened for curation rather than independently or domain reviewed; inclusion is contextual, not automatic claim evidence."
      }
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    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20190002449",
      "title": "The K Dwarf Advantage for Biosignatures on Directly Imaged Exoplanets",
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      "snapshot": {
        "id": "ntrs-20190002449",
        "title": "The K Dwarf Advantage for Biosignatures on Directly Imaged Exoplanets",
        "url": "https://ntrs.nasa.gov/citations/20190002449",
        "topic": "destinations-astrobiology",
        "year": 2019,
        "publishedAt": "2019-03-01T00:00:00.0000000+00:00",
        "authors": [
          "Arney, Giada N."
        ],
        "publisher": "IOPscience",
        "resourceType": "Reprint (Version printed in journal)",
        "access": "open full text",
        "abstract": "Oxygen and methane are considered to be the canonical biosignatures of modern Earth, and the simultaneous detection of these gases in a planetary atmosphere is an especially strong biosignature. However, these gases may be challenging to detect together in the planetary atmospheres because photochemical oxygen radicals destroy methane. Previous work has shown that the photochemical lifetime of methane in oxygenated atmospheres is longer around M dwarfs, but M dwarf planet habitability may be hindered by extreme stellar activity and evolution. Here, we use a 1D photochemical-climate model to show that K dwarf stars also offer a longer photochemical lifetime of methane in the presence of oxygen compared to G dwarfs. For example, we show that a planet orbiting a K6V star can support about an order of magnitude more methane in its atmosphere compared to an equivalent planet orbiting a G2V star. In the reflected-light spectra of worlds orbiting K dwarf stars, strong oxygen and methane features could be observed at visible and near-infrared wavelengths. Because K dwarfs are dimmer than G dwarfs, they offer a better planet-star contrast ratio, enhancing the signal-to-noise ratio (S/N) possible in a given observation. For instance, a 50 hr observation of a planet at 7 pc with a 15 m telescope yields S/N = 9.2 near 1 m for a planet orbiting a solar-type G2V star, and S/N = 20 for the same planet orbiting a K6V star. In particular, nearby mid-late K dwarfs such as 61 Cyg A/B, Epsilon Indi, Groombridge 1618, and HD 156026 may be excellent targets for future biosignature searches.",
        "keywords": [],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “The K Dwarf Advantage for Biosignatures on Directly Imaged Exoplanets” covers Oxygen and methane are considered to be the canonical biosignatures of modern Earth, and the simultaneous detection of; it materially informs GShips work on biosignatures and target characterization.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "biosignatures-and-target-characterization",
        "evidenceBoundary": "NTRS provides open full text, but this reprint (version printed in journal) was screened for curation rather than independently or domain reviewed; inclusion is contextual, not automatic claim evidence."
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    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20200003064",
      "title": "Surviving and Thriving in Space and on Earth's Oceans - Human Logistics and Sustainability Comparisons and Considerations",
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      "snapshot": {
        "id": "ntrs-20200003064",
        "title": "Surviving and Thriving in Space and on Earth's Oceans - Human Logistics and Sustainability Comparisons and Considerations",
        "url": "https://ntrs.nasa.gov/citations/20200003064",
        "topic": "assembly-logistics",
        "year": 2020,
        "publishedAt": "2020-04-24T04:00:00.0000000+00:00",
        "authors": [
          "Robert P Mueller",
          "Kalepa Baybayan",
          "John Hamilton"
        ],
        "publisher": "Kennedy Space Center",
        "resourceType": "Abstract",
        "access": "open full text",
        "abstract": "The human species has a yearning for exploration as evidenced by the extensive historical ocean voyages and expeditions which have led to a massive advancement in the scientific and geodetic knowledge about planet Earth. These global explorations via the oceans have also had strategic, economic, cultural and religious implications and impacts, which have drastically changed the state of humanity and its condition.  The transportation network created by ships traveling  across the oceans has been supplemented by other transportation networks on land and in the air, creating a global economy that, in general, has improved the human condition leading to better health, longer lives, lower child mortality, better education, political freedom, higher gross national product (GNP) and improved hygiene.  The logical extension of this societal trend is to extend the transportation network and human civilization into outer space, beyond the cradle of planet Earth. Our solar system contains vast amounts of natural resources which can be harnessed and used to bootstrap a space economy and related infrastructure by using advanced technologies.\n\nSailing journeys from hundreds of years ago required large vessels and large crews, (in comparison with today’s space capsules). Modern sailors of today are able to complete large voyages, in small vessels, with a minimal crew, comparable in magnitude to modern space travel.  This paper will use a systems engineering approach (e.g. using the NASA Human Integration Design Handbook (HIDH), NASA-SP-2010-3407, 2010 and the “Advanced Life Support Baseline Values and Assumptions Document, (BVAD)” NASA-CR-2004-208941, 2004.), to examine and compare the logistics and sustainability aspects of a small crew traveling on Earth's oceans in sailing vessels versus humans traveling in space. The “Mālama Honua Worldwide Voyage” of the Hokule’a, a replica of an ancient Hawaiian double hulled sailing canoe, will be used as a case study. This is the best comparison case since the Polynesian exploration of the vast (and virtually empty) Pacific Ocean is the closest analogue to modern space travel. “\"Both are voyages of exploration.” –Shuttle astronaut Lacy Veach. Minimizing waste and maximizing re-use and re-cycling will lead to more efficient logistics and sustainability. In addition, In-Situ Resource Utilization (ISRU) strategies, based on successful Earth based strategies used for many years by sailors will be considered and evaluated for their usefulness. For example, human logistics for a typical space mission are shown in Table 1 and Table 2 (Lopez et al, 2015). Studies show that typical human water consumption in space is projected to be 3.2 kg/day per crew member as shown in Table 2.  Data from human sailing voyages around the globe will be examined. Anecdotal evidence indicates that knowledgeable and well-equipped modern sailors, who conserve water, can comfortably live using 1.5 to 5 kg/day per person. This paper will investigate key logistics and sustainability aspects of living in space and compare them quantitatively to similar aspects of living on ocean faring sailing vessels on Earth. Mutually beneficial observations, advanced technologies and modern considerations will be applied within confines of a remote sailing environment, which could be of immense value to both the space faring community and the ocean sailing community.\n",
        "keywords": [
          "Space",
          "Sustainability",
          "Oceans",
          "Logistics",
          "Exploration",
          "Earth",
          "Sailing"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “Surviving and Thriving in Space and on Earth's Oceans - Human Logistics and Sustainability Comparisons and Considerations” covers Space, Sustainability, Oceans, Logistics; it materially informs GShips work on earth space logistics.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "earth-space-logistics",
        "evidenceBoundary": "NTRS provides open full text, but this abstract was screened for curation rather than independently or domain reviewed; inclusion is contextual, not automatic claim evidence."
      }
    },
    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20210003835",
      "title": "Mechanical Pumped Cooling Loop for Spacecraft Thermal Control",
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      "snapshot": {
        "id": "ntrs-20210003835",
        "title": "Mechanical Pumped Cooling Loop for Spacecraft Thermal Control",
        "url": "https://ntrs.nasa.gov/citations/20210003835",
        "topic": "power-thermal",
        "year": 1996,
        "publishedAt": "1996-07-08T00:00:00.0000000+00:00",
        "authors": [
          "Gram, Marshall B.",
          "Birur, Gajanana C.",
          "Bhandari, Pradeep"
        ],
        "publisher": "Jet Propulsion Laboratory",
        "resourceType": "Other",
        "access": "open metadata",
        "abstract": "The Mars Pathfinder (MPF) spacecraft, scheduled for a December '96 launch to Mars, uses a mechanically pumped loop to transfer dissipated heat from the insulated lander electronics to an external radiator. This paper discusses the tradeoffs performed before choosing a mechanically pumped loop as the thermal control system for MPF. It describes the analysis, design, and predicted performance of this system. The various development tests performed are discussed along with the current status of this cooling system. Finally, some thoughts on the development of mechanically pumped loops for future spacecraft are presented.",
        "keywords": [
          "Mars",
          "Pathfinder",
          "thermal",
          "control",
          "mechanical",
          "pumps",
          "cooling",
          "systems"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated as a flown-program precursor describing Mars Pathfinder's mechanically pumped cooling-loop trade, analysis, design, development tests, and predicted performance.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "thermal control",
        "evidenceBoundary": "Only NTRS metadata and an abstract are open here; the complete test record and flight performance were not validated in this pass. It is bounded spacecraft precedent, not worldship thermal-closure evidence."
      }
    },
    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20210010209",
      "title": "Habitability of Cloudy Worlds: Intersecting Constraints and Unknowns",
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      "snapshot": {
        "id": "ntrs-20210010209",
        "title": "Habitability of Cloudy Worlds: Intersecting Constraints and Unknowns",
        "url": "https://ntrs.nasa.gov/citations/20210010209",
        "topic": "destinations-astrobiology",
        "year": 2021,
        "publishedAt": "2021-03-20T07:00:00.0000000+00:00",
        "authors": [
          "D. M. Gentry",
          "L. Iraci",
          "E. Barth",
          "K. McGouldrick",
          "K.-L. Jessup"
        ],
        "publisher": "Ames Research Center",
        "resourceType": "Conference Paper",
        "access": "open metadata",
        "abstract": "\"Follow the water\" has long been a theme  of  astrobiology.   Where  there  are  terrestrial worlds with water, there are likely to be clouds.  Earth's clouds carry active microbes, in addition to inactive life that comprises a significant minority of dry dust.  Both  Venus  and  Mars  are  believed  to  have  had significant  early  water;  on  Venus,  the  limited  water retained in the clouds has been suggested as a potential refuge for life, a parallel to Mars's subsurface water.  Conversely, as microbes on Earth do not stay airborne for  very  long, a hypothetical  exoplanet with  more persistent cloud cover could be even more favorable to an airborne biosphere than Earth. Airborne microbiology is significant at a planetary scale for Earth.  Effects include weather (microbes as condensation  and  ice  nuclei),  climate  (alteration  of cloud and surface albedo), and water and air chemistry (through  metabolic  processing). Some  of  these effects,  if  present  on  exoplanets,  could  be  detectable through  remote  observation. Understanding  the parameters that constrain the habitability of clouds is therefore necessary to help guide the search for life.\n\nPaper includes the extended abstract.",
        "keywords": [
          "Habitability",
          "Cloudy",
          "Worlds",
          "Physical Constraints",
          "Unknowns"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “Habitability of Cloudy Worlds: Intersecting Constraints and Unknowns” covers Habitability, Cloudy, Worlds, Physical Constraints; it materially informs GShips work on planetary habitability modeling.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "planetary-habitability-modeling",
        "evidenceBoundary": "NTRS provides metadata and an abstract, not reviewed full text; methods, results, and current applicability remain unverified. Inclusion is contextual, not automatic claim evidence."
      }
    },
    {
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      "recordId": "ntrs-20230018678",
      "title": "Interstellar Propulsion",
      "publicPath": "/atlas/ntrs-20230018678",
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      "snapshot": {
        "id": "ntrs-20230018678",
        "title": "Interstellar Propulsion",
        "url": "https://ntrs.nasa.gov/citations/20230018678",
        "topic": "propulsion",
        "year": 2024,
        "publishedAt": "2024-06-01T05:00:00.0000000+00:00",
        "authors": [
          "Michael R Lapointe"
        ],
        "publisher": "Elsevier",
        "resourceType": "Book Chapter",
        "access": "open full text",
        "abstract": "As you read this, humanity’s first interstellar probe has left our solar system and is moving at nearly 17 km/s on its journey through interstellar space. Launched in 1977 and carrying a message from Earth on an inscribed golden disk, Voyager 1 completed its grand tour of the outer planets and has since travelled more than 24 billion km on its outward journey; it’s twin probe, Voyager 2, has also left the heliopause and entered interstellar space, traveling over 20 billion km from Earth. Yet even at these speeds and distances, our intrepid Voyagers have barely moved beyond the influence of our local star. If the distance between our Sun and the closest neighboring star system, Alpha Centauri, were scaled to the size of a meter stick, Voyager 1 would be located just over the ½-mm mark, having traveled 0.06% of the way to the next star (assuming it was pointed in the right direction, which it isn’t). At this rate it will take the probe nearly 75 thousand years to cover the equivalent distance to Alpha Centauri.",
        "keywords": [
          "Interstellar",
          "Propulsion"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated as a recent book-chapter overview linking Voyager-scale speeds to the propulsion and energy gap for meaningful interstellar missions.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "interstellar propulsion",
        "evidenceBoundary": "NTRS lists open full text, but this pass screened metadata and abstract rather than independently reviewing each propulsion comparison. It is synthesis context, not automatic evidence for feasibility."
      }
    },
    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20250005083",
      "title": "In-Time Aviation Safety Management Systems for Increasingly Autonomous Wildland Firefighting Operations",
      "publicPath": "/atlas/ntrs-20250005083",
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      "snapshot": {
        "id": "ntrs-20250005083",
        "title": "In-Time Aviation Safety Management Systems for Increasingly Autonomous Wildland Firefighting Operations",
        "url": "https://ntrs.nasa.gov/citations/20250005083",
        "topic": "ai-autonomy",
        "year": 2025,
        "publishedAt": "2025-05-28T04:00:00.0000000+00:00",
        "authors": [
          "Natasha Neogi"
        ],
        "publisher": "Langley Research Center",
        "resourceType": "Presentation",
        "access": "open full text",
        "abstract": "An In Time Aviation Safety Management System (IASMS) for wildland firefighting is a comprehensive approach to managing and controlling safety risks related to increasingly autonomous aviation operations in wildfire contexts. Elements of an IASMS include risk assessment and hazard identification, safety monitoring and control, safety policy and procedures, as well as learning and improvement.  The  IASMS concept assumes a set of enabling Services, Functions, and Capabilities (SFCs) will perform risk monitoring and support more timely safety risk assessment and mitigation. The IASMS concept is intended to be tailorable; that is, the set of enabling SFCs will vary due to the mission, vehicle platform(s), operational environment, and safety risk tolerance.  This talk will consider increasingly autonomous aviation operations that are in a mid-term context (i.e., 3-5 years from today) in medium-density air traffic (i.e., 10-15 aircraft).  Non-segregated operations are the desired state: Small UAS, large UAS, and crewed aircraft all safely operating different missions within the temporary flight restriction (TFR) airspace will need to be addressed.  The efficacy of in-time, operational risk mitigation of increasingly autonomous aviation operations will be explored as a path towards assuring these operations and enabling their deployment in the wildland firefighting ecosystem.  ",
        "keywords": [
          "increasingly autonomous systems",
          "in time safety management systems",
          "wildland firefighting"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “In-Time Aviation Safety Management Systems for Increasingly Autonomous Wildland Firefighting Operations” covers increasingly autonomous systems, in time safety management systems, wildland firefighting; it materially informs GShips work on autonomous safety management.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "autonomous-safety-management",
        "evidenceBoundary": "NTRS provides open full text, but this presentation was screened for curation rather than independently or domain reviewed; inclusion is contextual, not automatic claim evidence."
      }
    },
    {
      "recordType": "atlas-resource",
      "recordId": "ntrs-20250011179",
      "title": "Evaluation of Electrically Heated Nuclear Reactor Development Units for the Advancement of Propulsion and Power Technologies",
      "publicPath": "/atlas/ntrs-20250011179",
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        "id": "ntrs-20250011179",
        "title": "Evaluation of Electrically Heated Nuclear Reactor Development Units for the Advancement of Propulsion and Power Technologies",
        "url": "https://ntrs.nasa.gov/citations/20250011179",
        "topic": "power-thermal",
        "year": 2026,
        "publishedAt": "2026-04-27T05:00:00.0000000+00:00",
        "authors": [
          "Jackson Cho",
          "Jacob Ondeck",
          "Brian Hoang",
          "Matthew Hitt",
          "Tyler Dennis",
          "Noah Sutton"
        ],
        "publisher": "Marshall Space Flight Center",
        "resourceType": "Conference Paper",
        "access": "open full text",
        "abstract": "The national interest in sustainable nuclear power has seen a recent and significant resurgence, with targeted investments creating an enriched environment for the development of more modular and situational nuclear systems. Despite this, logistical and regulatory hurdles risk throttling reactor development efforts, with the potential of disproportionally affecting those technologies at the micro reactor scale. To permit rapid thermal testing of integrated reactor systems earlier in the development cycle, electric heating can be employed to simulate fission heating. The Nuclear Systems Team within Marshall Space Flight Center’s (MSFC) Propulsion Research and Technology Branch has expertise performing such non-nuclear testing to evaluate reactor components, inspect material compatibilities, and characterize thermal system performances. Tests of this type have been critically valuable to advancing space nuclear propulsion in their ability to validate fuel element materials and geometries in a simulated yet thermally representative nuclear thermal propulsion reactor environment. Similarly, this approach has been implemented by the team to the advancement of reactors with applicability to space nuclear propulsion. At Antares Industries, nuclear and system engineers are developing a special-purpose multi-Kilowatt scale micro-reactor for use in first response, and space, and other environments. Reactor architectures of this output scale readily lend themselves to the implementation of electrical demonstration units (EDU). Consequently, Antares and MSFC personnel have collaborated to develop a subscale EDU representative of the Antares R1 reactor system. Herein is a discussion of the design, buildup, and testing of the Antares EDU, alongside potential future work discussions of the advancement of micro-reactor non-nuclear development testing.",
        "keywords": [
          "Space Nuclear Propulsion",
          "Reactor Ground Testing",
          "Nuclear Electric Propulsion",
          "Fission Surface Power"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated for electrically heated reactor development units that decouple early thermal and integrated-system testing from fission operations while exposing regulatory and logistics constraints.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "nuclear test and assurance",
        "evidenceBoundary": "NTRS lists open full text, but curation relied on metadata and abstract and did not validate the test units or nuclear-safety case. It is civil test-method context, not reactor approval or claim evidence."
      }
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