{"project":{"acronym":"","projectId":94407,"title":"Developing Graphene Foil Technology for Instruments Targeting Low-Energy Ring Current Populations at Earth","primaryTaxonomyNodes":[{"taxonomyNodeId":10741,"taxonomyRootId":8816,"parentNodeId":10740,"level":3,"code":"TX08.1.1","title":"Detectors and Focal Planes","definition":"Detectors, focal planes and readout integrated circuits provide large-format array technologies that require high quantum efficiency (QE); low noise, high resolution, uniform, and stable response; low power and cost; and high reliability. These technologies include low-noise, high-speed, low-power and radiation hardened readout integrated circuit (ROIC) electronics; superconducting sensors; spectral detectors; polarization-sensitive detectors; radiation-hardened detectors; and micro-Kelvin and sub-Kelvin high sensitivity detectors that cover the spectrum from submillimeter wave (Far-IR) to X-ray.","exampleTechnologies":"Backshort Undergrid bolometer arrays, Mercury Cadmium Telluride and Strained Superlattice Arrays, charge coupled devices, sidecar readout integrated circuits, radiometric calibration and abnormality correction algorithms (e.g. non-uniformity)","hasChildren":false,"hasInteriorContent":true}],"startTrl":3,"currentTrl":3,"endTrl":4,"benefits":"Support NASA's Heliophysics strategic science objectives to understand the Sun and its interactions with Earth and the solar system, including space weather. This will be achieved by developing/demonstrating instrumentation technology necessary to address the following science goals: Explore the physical processes in the space environment from the Sun to the Earth and throughout the solar system; Advance our understanding of the connections that link the Sun, the Earth, planetary space environments, and the outer reaches of our solar system; Develop the knowledge and capability to detect and predict extreme conditions in space to protect life and society and to safeguard human and robotic explorers beyond Earth.","description":"The goal of this proposal is to develop graphene foil technology to the point where these foils can be readily used in energetic neutral atom (ENA) and plasma instruments in space that employ thin carbon foils. The science question targeted by this technology development is \"What is the contribution from Coulomb collisions to plasma loss from the Earth's ring current?\" Coulomb collisions between ring current ions and thermal populations in the plasmasphere are believed to produce a source of low energy (< 500 eV) ions to the Earth's inner magnetosphere during both quiet and active times. The ENAs produced from these low energy ions are difficult to measure with current ENA instruments because of their very low probability of being transmitted through the thin carbon foils (~0.5 ug cm^-2 or ~100 atomic layers) currently in use. The recent development of graphene, a two-dimensional carbon material where the atoms are tightly packed into a honeycomb lattice, has opened the possibility of making much thinner foils (few atomic layers) and, therefore, expanding the energy range of ENA imagers to colder particles. Developing this new technology can make it possible to remotely observe Coulomb-collision-generated sub-keV ring current populations via ENA imaging, along with low energy ENA populations from other sources. To achieve our goal, we propose the following three objectives, 1.\tDevelop large area (> 1 cm^2), single crystal graphene foils with controllable thickness (3 - 5 atomic layers). 2.\tCharacterize the properties of large area, single crystal graphene foils and their response to vibrational, thermal, and acoustic stresses. 3.\tCompare the performance of large area, single crystal graphene and thin carbon foils in a prototype ENA instrument. The graphene foils used in this project will be produced at Texas State University by Co-I Dr. Qingkai Yu. We will use polymer-assisted transfer of graphene from the copper substrate to electroformed nickel grids. The angular scattering and energy straggling of ions passing through the graphene foils will be measured using existing experimentsin the Ion Calibration Facility at Southwest Research Institute (SwRI). An experiment for measuring secondary electron emission will be built based on a setup built previously by Co-I Allegrini. Testing graphene and thin carbon foil performance in a prototype ENA instrument will be accomplished using an engineering model of the Two Wide-angle Imaging Neutral-atom Spectrometers (TWINS). All facilities, experiments, and instruments are available to this project. Our proposal directly responds to the NASA-ROSES 2017 H-TIDeS AO by developing technologies to enable the measurement of sub-keV ring current populations at Earth using ENA sensors. This new capability directly supports the science question \"How are magnetospheric and ionospheric plasma transported and accelerated by solar wind forcing and magnetosphere-ionosphere coupling?\" of the Magnetospheric Energetics, Dynamics, and Ionospheric Coupling (MECIDI) mission concept. MEDICI is a Solar Terrestrial Probes class mission that was recommended for implementation in the 2012 Decadal Strategy for Solar and Space Physics. The technologies developed here will also lead to measurements that respond to two key NASA Heliophysics Science goals, (1) Explore the physical processes in the space environment from the Sun to the Earth and throughout the solar system, and (2) Advance our understanding of the connections that link the Sun, the Earth, planetary space environments, and the outer reaches of our solar system.","destinations":[{"lkuCodeId":1545,"code":"SUN","description":"Sun","lkuCodeTypeId":526,"lkuCodeType":{"codeType":"DESTINATION_TYPE","description":"Destination Type"}}],"startYear":2018,"startMonth":2,"endYear":2023,"endMonth":12,"statusDescription":"Completed","principalInvestigators":[{"contactId":399117,"canUserEdit":false,"firstName":"Robert","lastName":"Ebert","fullName":"Robert W Ebert","fullNameInverted":"Ebert, Robert W","middleInitial":"W","primaryEmail":"rebert@swri.edu","publicEmail":false,"nacontact":false}],"programDirectors":[{"contactId":413940,"canUserEdit":false,"firstName":"Roshanak","lastName":"Hakimzadeh","fullName":"Roshanak Hakimzadeh","fullNameInverted":"Hakimzadeh, Roshanak","primaryEmail":"hakimzadeh@nasa.gov","publicEmail":true,"nacontact":false}],"programManagers":[{"contactId":413940,"canUserEdit":false,"firstName":"Roshanak","lastName":"Hakimzadeh","fullName":"Roshanak Hakimzadeh","fullNameInverted":"Hakimzadeh, Roshanak","primaryEmail":"hakimzadeh@nasa.gov","publicEmail":true,"nacontact":false}],"coInvestigators":[{"contactId":411552,"canUserEdit":false,"firstName":"Ronald","lastName":"Kalmbach","fullName":"Ronald B Kalmbach","fullNameInverted":"Kalmbach, Ronald B","middleInitial":"B","primaryEmail":"contracts@swri.org","publicEmail":false,"nacontact":false},{"contactId":155836,"canUserEdit":false,"firstName":"Frederic","lastName":"Allegrini","fullName":"Frederic Allegrini","fullNameInverted":"Allegrini, Frederic","primaryEmail":"fallegrini@swri.edu","publicEmail":false,"nacontact":false},{"contactId":379128,"canUserEdit":false,"firstName":"Qingkai","lastName":"Yu","fullName":"Qingkai Yu","fullNameInverted":"Yu, Qingkai","primaryEmail":"qingkai.yu@txstate.edu","publicEmail":false,"nacontact":false}],"website":"","libraryItems":[],"transitions":[],"responsibleMd":{"acronym":"SMD","canUserEdit":false,"city":"","external":false,"linkCount":0,"organizationId":4909,"organizationName":"Science Mission Directorate","organizationType":"NASA_Mission_Directorate","naorganization":false,"organizationTypePretty":"NASA Mission Directorate"},"program":{"acronym":"H-TIDeS","active":true,"description":"
Low Cost Access to Space (LCAS) investigations may be science investigations in and of themselves or proof-of-concept experiments for techniques/detectors that enable new Heliophysics science. LCAS includes rides on research balloons, sounding rockets, the International Space Station, commercial reusable suborbital rockets, and CubeSats. LCAS investigations that launch into space in order to return scientific data are expected to make direct contributions to the science of Heliophysics.
Instrument and Technology Development (ITD) investigations have as their objective the development of instrument technologies that show promise for use in scientific investigations on future Heliophysics science missions, including the development of laboratory instrument prototypes, but not of flight hardware. Instrument development proposals are not necessarily expected to apply the results of their efforts to science questions within the time period of the proposed effort. They must, however, demonstrate that there are specific scientific problem(s), for which the development is a necessary precursor.
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