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        "id": "ntrs-19890017516",
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        "authors": [
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        "abstract": "One of the elements of the Space Station Freedom power system is the Photovoltaic (PV) module. These modules will be assembled on-orbit during the assembly phase of the program. These modules will be assembled either from the shuttle orbiter or from the Mobile Servicing Center (MSC). The different types of assembly operations that will be used to assemble PV Modules are described.",
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        "verifiedAt": "2026-07-25",
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      "recordId": "ntrs-19920073222",
      "title": "The ITU as a means of facilitating international collaboration on space radiocommunication systems",
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        "id": "ntrs-19920073222",
        "title": "The ITU as a means of facilitating international collaboration on space radiocommunication systems",
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        "topic": "institutions-workforce",
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        "abstract": "The role of the International Telecommunication Union (ITU) in the international collaboration in the field of space radio communications is reviewed. The history of the ITU, its structure and activities, and the functions of the permanent organs of the ITU are briefly discussed. Attention is then given to new space service applications for communications around 400 MHz, space services near 2 GHz, new space service applications above 20 GHz, and links for future planetary missions. The discussion also covers deep space allocations near 32/34 GHz, space VLBI applications, new earth exploration satellite service applications, and future work.",
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        "authors": [
          "Birur, Gajanana C.",
          "Siebes, Georg",
          "Swanson, Theodore D.",
          "Powers, Edward I."
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        "abstract": "Thermal control of the spacecraft is typically achieved by removing heat from the spacecraft parts that tend to overheat and adding heat to the parts that tend get too cold. The equipment on the spacecraft can get very hot if it is exposed to the sun or have internal heat generation. The pans also can get very cold if they are exposed to the cold of deep space. The spacecraft and instruments must be designed to achieve proper thermal balance. The combination of the spacecraft's external thermal environment, its internal heat generation (i.e., waste heat from the operation of electrical equipment), and radiative heat rejection will determine this thermal balance. It should also be noted that this is seldom a static situation, external environmental influences and internal heat generation are normally dynamic variables which change with time. Topics discussed include thermal control system components, spacecraft mission categories, spacecraft thermal requirements, space thermal environments, thermal control hardware, launch and flight operations, advanced technologies for future spacecraft,",
        "keywords": [],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated as a foundational spacecraft thermal-control overview of heat removal and addition, external environment, internal dissipation, insulation, radiators, heaters, and system balance.",
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        "id": "ntrs-20040089477",
        "title": "Vertebrate development in the environment of space:  models, mechanisms, and use of the medaka",
        "url": "https://ntrs.nasa.gov/citations/20040089477",
        "topic": "reproduction-genetics",
        "year": 1997,
        "publishedAt": "1997-06-01T00:00:00.0000000+00:00",
        "authors": [
          "Wolgemuth, D. J.",
          "Herrada, G.",
          "Kiss, S.",
          "Cannon, T.",
          "Forsstrom, C.",
          "Pranger, L. A.",
          "Weismann, W. P.",
          "Pearce, L."
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        "publisher": "Ames Research Center",
        "resourceType": "Reprint (Version printed in journal)",
        "access": "open metadata",
        "abstract": "With the advent of space travel, it is of immediate interest and importance to study the effects of exposure to various aspects of the altered environment of space, including microgravity, on Earth-based life forms. Initial studies of space travel have focused primarily on the short-term effects of radiation and microgravity on adult organisms. However, with the potential for increased lengths of time in space, it is critical to now address the effects of space on all phases of an organism's life cycle, from embryogenesis to post-natal development to reproduction. It is already possible for certain species to undergo multiple generations within the confines of the Mir Space Station. The possibility now exists for scientists to consider the consequences of even potentially subtle defects in development through multiple phases of an organism's life cycle, or even through multiple generations. In this discussion, we highlight a few of the salient observations on the effects of the space environment on vertebrate development and reproductive function. We discuss some of the many unanswered questions, in particular, in the context of the choice of appropriate models in which to address these questions, as well as an assessment of the availability of hardware already existing or under development which would be useful in addressing these questions.",
        "keywords": [
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          "NASA Discipline Developmental Biology",
          "manned",
          "STS-70 Shuttle Project",
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          "Female",
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          "Male",
          "Gene Expression Regulation, Developmental",
          "Temperature"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated for medaka fish as a compact vertebrate model of development and reproduction in space, with relevance to autonomous aquatic research systems.",
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      "title": "Johnson Space Center's Regenerative Life Support Systems Test Bed",
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      "snapshot": {
        "id": "ntrs-20040089896",
        "title": "Johnson Space Center's Regenerative Life Support Systems Test Bed",
        "url": "https://ntrs.nasa.gov/citations/20040089896",
        "topic": "life-support",
        "year": 1996,
        "publishedAt": "1996-01-01T00:00:00.0000000+00:00",
        "authors": [
          "Barta, D. J.",
          "Henninger, D. L."
        ],
        "publisher": "Legacy CDMS",
        "resourceType": "Reprint (Version printed in journal)",
        "access": "open metadata",
        "abstract": "The Regenerative Life Support Systems (RLSS) Test Bed at NASA's Johnson Space Center is an atmospherically closed, controlled environment facility for human testing of regenerative life support systems using higher plants in conjunction with physicochemical life support systems.  The facility supports NASA's Advanced Life Support (ALS) Program.  The facility is comprised of two large scale plant growth chambers, each with approximately 11 m2 growing area.  The root zone in each chamber is configurable for hydroponic or solid media plant culture systems.  One of the two chambers, the Variable Pressure Growth Chamber (VPGC), is capable of operating at lower atmospheric pressures to evaluate a range of environments that may be used in a planetary surface habitat; the other chamber, the Ambient Pressure Growth Chamber (APGC) operates at ambient atmospheric pressure.  The air lock of the VPGC is currently being outfitted for short duration (1 to 15 day) human habitation at ambient pressures.  Testing with and without human subjects will focus on 1) integration of biological and physicochemical air and water revitalization systems; 2) effect of atmospheric pressure on system performance; 3) planetary resource utilization for ALS systems, in which solid substrates (simulated planetary soils or manufactured soils) are used in selected crop growth studies; 4) environmental microbiology and toxicology; 5) monitoring and control strategies; and 6) plant growth systems design.  Included are descriptions of the overall design of the test facility, including discussions of the atmospheric conditioning, thermal control, lighting, and nutrient delivery systems.",
        "keywords": [
          "NASA Discipline Number 61-10",
          "NASA Program Advanced Life Support",
          "NASA Center JSC",
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        ],
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        "selectionNote": "Curated because this 1996 reprint (version printed in journal) from Legacy CDMS specifically covers “Johnson Space Center's Regenerative Life Support Systems Test Bed”; its abstract describes The Regenerative Life Support Systems (RLSS) Test Bed at NASA's Johnson Space Center is an atmospherically closed, controlled environment facility for human testing of… This materially informs GShips regenerative life support.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "regenerative life support",
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      "title": "A Systems Engineering Approach to Architecture Development",
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      "snapshot": {
        "id": "ntrs-20150004445",
        "title": "A Systems Engineering Approach to Architecture Development",
        "url": "https://ntrs.nasa.gov/citations/20150004445",
        "topic": "institutions-workforce",
        "year": 2015,
        "publishedAt": "2015-07-13T00:00:00.0000000+00:00",
        "authors": [
          "David A. Di Pietro"
        ],
        "publisher": "Goddard Space Flight Center",
        "resourceType": "Conference Paper",
        "access": "open full text",
        "abstract": "Architecture development is often conducted prior to system concept design when there is a need to determine the best-value mix of systems that works collectively in specific scenarios and time frames to accomplish a set of mission area objectives. While multiple architecture frameworks exist, they often require use of unique taxonomies and data structures. In contrast, this paper characterizes architecture development using terminology widely understood within the systems engineering community. Using a notional civil space architecture example, it employs a multi-tier framework to describe the enterprise level architecture and illustrates how results of lower tier, mission area architectures integrate into the enterprise architecture. It also presents practices for conducting effective mission area architecture studies, including establishing the trade space, developing functions and metrics, evaluating the ability of potential design solutions to meet the required functions, and expediting study execution through the use of iterative design cycles.",
        "keywords": [
          "Multi-tier Framework",
          "Systems Engineering",
          "Architecture Development"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because this 2015 conference paper from Goddard Space Flight Center specifically covers “A Systems Engineering Approach to Architecture Development”; its abstract describes Architecture development is often conducted prior to system concept design when there is a need to determine the best-value mix of systems that works collectively in… This materially informs GShips institutions and workforce.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "institutions and workforce",
        "evidenceBoundary": "NTRS lists open full text, but this pass assessed catalog metadata and abstract rather than independently validating the document. Inclusion is contextual discovery support, not automatic evidence for a GShips claim."
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      "recordId": "ntrs-20170000778",
      "title": "Detection of DNA Damage by Space Radiation in Human Fibroblasts Flown on the International Space Station",
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        "id": "ntrs-20170000778",
        "title": "Detection of DNA Damage by Space Radiation in Human Fibroblasts Flown on the International Space Station",
        "url": "https://ntrs.nasa.gov/citations/20170000778",
        "topic": "radiation-environment",
        "year": 2017,
        "publishedAt": "2017-01-23T00:00:00.0000000+00:00",
        "authors": [
          "Lu, Tao",
          "Zhang, Ye",
          "Wong, Michael",
          "Feiveson, Alan",
          "Gaza, Ramona",
          "Stoffle, Nicholas",
          "Wang, Huichen ",
          "Wilson, Bobby"
        ],
        "publisher": "Johnson Space Center",
        "resourceType": "Presentation",
        "access": "open full text",
        "abstract": "Space radiation consists of energetic charged particles of varying charges and energies. Exposure of astronauts to space radiation on future long duration missions to Mars, or missions back to the Moon, is expected to result in deleterious consequences such as cancer and comprised central nervous system (CNS) functions. Space radiation can also cause mutation in microorganisms, and potentially influence the evolution of life in space. Measurement of the space radiation environment has been conducted since the very beginning of the space program. Compared to the quantification of the space radiation environment using physical detectors, reports on the direct measurement of biological consequences of space radiation exposure have been limited, due primarily to the low dose and low dose rate nature of the environment. Most of the biological assays fail to detect the radiation effects at acute doses that are lower than 5 centiSieverts. In a recent study, we flew cultured confluent human fibroblasts in mostly G1 phase of the cell cycle to the International Space Station (ISS). The cells were fixed in space after arriving on the ISS for 3 and 14 days, respectively. The fixed cells were later returned to the ground and subsequently stained with the gamma-H2AX (Histone family, member X) antibody that are commonly used as a marker for DNA damage, particularly DNA double strand breaks, induced by both low-and high-linear energy transfer radiation. In our present study, the gamma-H2AX (Histone family, member X) foci were captured with a laser confocal microscope. To confirm that some large track-like foci were from space radiation exposure, we also exposed, on the ground, the same type of cells to both low-and high-linear energy transfer protons, and high-linear energy transfer Fe ions. In addition, we exposed the cells to low dose rate gamma rays, in order to rule out the possibility that the large track-like foci can be induced by chronic low-linear energy transfer radiation.",
        "keywords": [],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated for an ISS fibroblast experiment examining DNA damage and repair signatures after combined spaceflight conditions, relevant to cellular-risk methods and biospecimen design.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "cellular radiation response",
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      "title": "Biosignature False Positives",
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        "id": "ntrs-20180004768",
        "title": "Biosignature False Positives",
        "url": "https://ntrs.nasa.gov/citations/20180004768",
        "topic": "destinations-astrobiology",
        "year": 2018,
        "publishedAt": "2018-04-12T00:00:00.0000000+00:00",
        "authors": [
          "Harman, Chester E.",
          "Domagal-Goldman, Shawn"
        ],
        "publisher": "Springer International Publishing ",
        "resourceType": "Book Chapter",
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        "abstract": "In our search for life - whether within the earliest part of Earth's geologic record, on planets within our solar system such Mars, or especially for extrasolar planets - we must infer the presence of life from its impact on the local or global environment. These \"biosignatures,\" often identified from the known influence of terrestrial organisms on the Earth's atmosphere and surface, could be misdiagnosed when we apply them to alien worlds. The so-called false positives may occur when another process or suite of processes masks or mimics a biosignature. Here, we examine several leading biosignatures, then introduce potential false positives for these signals, and finally discuss methods to discriminate between the two using current and future detection technologies. We conclude that it is the astrobiology community's responsibility to thoroughly exhaust all possibilities before we resort to \"life\" as an explanation.",
        "keywords": [],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated because “Biosignature False Positives” covers In our search for life - whether within the earliest part of Earth's geologic record, on planets within; 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 book chapter was screened for curation rather than independently or domain reviewed; inclusion is contextual, not automatic claim evidence."
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      "title": "The Fusion Driven Rocket: Nuclear Propulsion through Direct Conversion of Fusion Energy",
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        "id": "ntrs-20190001178",
        "title": "The Fusion Driven Rocket: Nuclear Propulsion through Direct Conversion of Fusion Energy",
        "url": "https://ntrs.nasa.gov/citations/20190001178",
        "topic": "propulsion",
        "year": 2018,
        "publishedAt": "2018-11-12T00:00:00.0000000+00:00",
        "authors": [
          "Slough, John T."
        ],
        "publisher": "Headquarters",
        "resourceType": "Other",
        "access": "open full text",
        "abstract": "The future of manned space exploration and development of space depends critically on the creation of a dramatically more efficient propulsion architecture for in-space transportation. A very persuasive reason for investigating the applicability of nuclear power in rockets is the vast energy density gain of nuclear fuel when compared to chemical combustion energy. The Fusion Driven rocket (FDR) represents a revolutionary approach to fusion propulsion where the power source releases its energy directly into the propellant, not requiring conversion to electricity. It employs a solid lithium propellant that requires no significant tankage mass. The propellant is rapidly heated and accelerated to high exhaust velocity (> 30 km/s), while having no substantial physical interaction with the spacecraft thereby avoiding damage to the rocket and limiting both the thermal heat load and radiator mass. The key to achieving this stems from research at MSNW and the UW on the magnetically driven implosion of metal foils onto a magnetized plasma target to obtain fusion conditions. A logical extension of this work leads to a method that utilizes these metal shells (or liners) to not only achieve fusion conditions, but to serve as the propellant as well. Several low-mass, magnetically driven metal liners are inductively driven to converge radially and axially and form a thick blanket surrounding the target plasmoid and compress the plasmoid to fusion conditions. Virtually all of the radiant, neutron and particle energy from the plasma is absorbed by the encapsulating, thick metal blanket thereby isolating the spacecraft from the fusion. This energy, in addition to the intense Ohmic heating at peak magnetic field compression, is adequate to vaporize and ionize the metal blanket. The expansion of this hot, ionized metal propellant through a magnetically insulated nozzle produces high thrust at the optimal Isp. The energy from the fusion process, along with the waste heat, is thus utilized at very high efficiency. The basic scheme for FDR is illustrated and described in the report (see Fig. 2) The two most critical issues in meeting challenges introduced employing magneto-inertial fusion as the power source is driver efficiency and “stand-off” – the ability to isolate and protect fusion and thruster from the resultant fusion energy. By employing metal shells for compression, it is possible to produce the desired convergent motion inductively by inserting the metal sheets along the inner surface of cylindrical or conically tapered coils. Both stand-off and energy efficiency issues are solved by this arrangement. 3 This two year effort focused on achieving three key criteria for the Fusion Driven Rocket to move forward for technological development: (1) the physics of the FDR must be fully understood and validated, (2) the design and technology development for the FDR required for its implementation in space must be fully characterized, and (3) an in-depth analysis of the rocket design and spacecraft integration as well as mission architectures enabled by the FDR need to be performed. A subscale, laboratory liner compression test facility was assembled at the University of Washington Plasma Dynamics Laboratory with sufficient liner kinetic energy (~ 0.5 MJ) to reach conditions required for fusion breakeven conditions. Detailed experimental studies of the dynamic behavior of the driven liners as well as liner convergence and magnetic compression were performed. The development of both the 1D liner dynamics code and the full 3D ANSYS® liner calculations was achieved. The characterization of both the FDR and spacecraft as well as a design architecture analysis was conducted that included an examination of a wide range of mission architectures and destinations for which this fusion propulsion system would be enabling or critical. In particular a rapid, single launch manned Mars mission was developed.",
        "keywords": [
          "Energy",
          "Propulsion",
          "Fusion",
          "Engine",
          "Rocket",
          "Mission",
          "Exploration",
          "Launch"
        ],
        "sourceClass": "editor-selected-context",
        "selectionNote": "Curated for the Fusion Driven Rocket's direct conversion of fusion energy into propellant impulse and its claimed architecture advantages and mission dependencies.",
        "verifiedAt": "2026-07-25",
        "curationTopic": "fusion propulsion",
        "evidenceBoundary": "NTRS lists open full text, but the concept does not establish net fusion energy, flight hardware, safety, or achievable performance. It is speculative civil propulsion context, not evidence of readiness."
      }
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        "year": 2024,
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        "selectionNote": "Current institutional description of plasma, charging, high-voltage, electrostatic-discharge, electromagnetic-interference, radiation, and materials effects on spacecraft.",
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      "title": "Water Recycle System in an Artificial Closed Ecosystem — Lunar Palace 1: Treatment Performance and Microbial Evolution",
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        "title": "Water Recycle System in an Artificial Closed Ecosystem — Lunar Palace 1: Treatment Performance and Microbial Evolution",
        "url": "https://doi.org/10.1016/j.scitotenv.2021.151370",
        "topic": "reviewed-claim-source",
        "year": 2022,
        "authors": [
          "Ting Zhao",
          "Guanghui Liu",
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          "Yue Yi",
          "Beizhen Xie",
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        "publisher": "Science of the Total Environment",
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        "evidenceBoundary": "This stable source is used by at least one editorially assessed claim. Its claim-specific relation and locator—not Atlas inclusion—define the evidence use; independent domain review remains pending."
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        "verifiedAt": "2026-07-26",
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